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(1)
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(5)
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(1)
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(6)
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(1)
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(2)
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(9)
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(1)
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(1)
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(47)
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(2)
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(1)
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(1)
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(1)
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(2)
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(1)
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(1)
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(6)
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(3)
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(1)
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(5)
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(1)
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(1)
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(1)
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(9)
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(1)
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(1)
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(1)
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(1)
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(1)
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(1)
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(1)
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(1)
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(1)
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(1)
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(1)
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(1)
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(1)
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(1)
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(1)
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(1)
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(31)
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(1)
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(1)
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(3)
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(1)
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(1)
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(2)
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(1)
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(1)
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(4)
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(1)
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(1)
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(1)
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(1)
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(1)
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(1)
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(1)
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(1)
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(1)
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(1)
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(1)
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(1)
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(1)
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(1)
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(1)
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(9)
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(1)
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08-24-1956
(1)
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(4)
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(1)
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(1)
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(1)
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(1)
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(6)
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08-27-1965
(2)
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08-27-1975
(1)
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(1)
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(1)
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(78)
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(2)
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(1)
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(1)
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08-28-1987
(1)
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(8)
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(1)
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(8)
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(3)
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08-30-1928
(1)
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(1)
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(8)
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(1)
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(1)
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(1)
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(1)
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(7)
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08/01/02
(3)
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(1)
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(1)
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(1)
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(1)
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(1)
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09-01-1992
(3)
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(1)
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(1)
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09-01-1998
(18)
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(10)
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(1)
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09-03-1929
(7)
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(1)
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(1)
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(1)
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(1)
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(45)
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(1)
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(1)
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(1)
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(9)
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(2)
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(1)
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(1)
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09-12-1940
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(1)
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(1)
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(1)
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09-14-1923
(1)
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09-14-1944
(2)
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(1)
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(1)
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(1)
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(1)
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(1)
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(1)
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(1)
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(1)
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(1)
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(1)
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(5)
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(11)
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(1)
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(1)
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(1)
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(5)
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(26)
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(4)
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09-21-1994
(1)
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(15)
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(1)
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(1)
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(1)
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(1)
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(1)
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(1)
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(1)
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(1)
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(1)
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(1)
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(4)
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(1)
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(1)
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(2)
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(2)
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(1)
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(15)
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(1)
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(3)
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(1)
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09/17/03
(2)
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(2)
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1-1-1958
(1)
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(1)
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(1)
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(1)
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(1)
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1/13/09
(1)
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1/21/09
(3)
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1/22/09
(2)
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1/26/09
(1)
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1/29/09
(6)
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1/30/09
(3)
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1/5/09
(9)
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1/6/09
(10)
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1/7/09
(1)
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1/8/09
(5)
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10-01-1936
(1)
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(1)
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(1)
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(1)
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(1)
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(6)
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(1)
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(1)
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(1)
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(1)
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(2)
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(1)
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(2)
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(1)
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10-03-2004
(9)
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10-04-1932
(1)
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(3)
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(1)
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(1)
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(1)
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(1)
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10-05-1972
(1)
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(1)
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(1)
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10-06-1942
(1)
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(1)
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(5)
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(8)
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10-07-1991
(1)
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(1)
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(1)
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(1)
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(1)
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(1)
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(1)
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10-10-1939
(1)
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(1)
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10-10-2000
(10)
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10-11-1939
(3)
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10-11-1943
(1)
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10-11-1961
(1)
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10-11-1966
(1)
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10-11-1994
(1)
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(19)
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10-12-1926
(1)
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10-12-1928
(4)
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10-12-1937
(1)
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(1)
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(1)
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10-12-1984
(1)
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(1)
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(9)
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10-13-1925
(1)
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10-13-1992
(1)
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(1)
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10-13-1998
(4)
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(1)
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(2)
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(1)
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(1)
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(2)
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(2)
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(1)
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10-15-1984
(1)
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(1)
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(1)
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(2)
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(1)
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(2)
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(8)
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10-18-1923
(1)
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10-18-1962
(2)
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(1)
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(1)
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10-19-1940
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(1)
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(1)
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(1)
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(1)
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(4)
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(4)
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10-20-2000
(131)
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10-21-1999
(1)
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(1)
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(7)
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(1)
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(1)
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(7)
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(1)
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(1)
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(1)
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(1)
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(3)
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(1)
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(1)
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(1)
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(1)
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(1)
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(1)
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(1)
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(1)
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(12)
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(1)
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(1)
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(1)
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(1)
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(1)
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(5)
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(1)
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(1)
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(2)
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10th Century
(1)
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11 April 1991
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11 April 1996
(4)
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11 December 196
(8)
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11 October 1994
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11 September 20
(2)
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11-01-1940
(1)
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11-01-1949
(1)
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11-01-1951
(1)
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11-01-1963
(2)
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11-01-1972
(1)
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11-01-1982
(1)
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11-01-1987
(1)
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11-01-1989
(1)
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11-01-1990
(3)
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11-01-1991
(2)
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11-01-1994
(1)
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11-01-1995
(3)
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11-01-1996
(8)
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11-01-1997
(1)
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11-01-1998
(13)
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11-01-1999
(9)
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11-02-1925
(1)
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11-02-1962
(1)
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11-02-1964
(1)
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11-02-1998
(2)
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11-02-2000
(9)
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11-03-1992
(1)
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11-04-1938
(2)
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11-04-1941
(1)
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11-04-1997
(2)
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11-04-1998
(11)
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11-05-1928
(2)
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11-05-1941
(1)
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11-05-1959
(1)
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11-05-1998
(4)
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11-06-1949
(1)
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11-07-1941
(1)
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(1)
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11-07-1962
(3)
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11-07-1997
(8)
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11-08-1937
(1)
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11-08-1940
(1)
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11-08-1999
(1)
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11-08-2000
(4)
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11-09-1989
(1)
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11-09-2001
(6)
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11-10-1961
(1)
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11-10-1996
(7)
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11-11-1911
(1)
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11-11-1931
(1)
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11-11-1960
(7)
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11-11-1963
(6)
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11-11-1970
(9)
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11-11-1971
(1)
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11-11-1975
(5)
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(2)
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(3)
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11-12-1965
(1)
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11-12-1995
(1)
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11-12-1997
(21)
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11-13-1928
(1)
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11-13-1961
(1)
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11-13-1967
(1)
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11-13-1995
(7)
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(10)
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11-14-1941
(2)
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11-14-1945
(1)
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11-14-1989
(3)
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(2)
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(2)
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11-14-1996
(1)
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11-14-2001
(9)
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11-14-90
(1)
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(1)
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(1)
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(1)
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(1)
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(1)
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(1)
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11-15-2002
(1)
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(1)
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11-16-1963
(1)
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(1)
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11-16-1994
(1)
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(2)
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11-17-1969
(1)
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11-17-1986
(2)
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(1)
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11-17-1994
(1)
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(4)
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(1)
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(1)
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(1)
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(1)
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(1)
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(1)
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11-18-1999
(2)
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(4)
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11-19-1987
(1)
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(13)
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(2)
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(1)
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11-20-1943
(1)
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(1)
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(2)
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(1)
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(1)
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(2)
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(2)
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11-21-1962
(1)
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(3)
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11-21-1997
(9)
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(4)
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11-22-1989
(1)
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11-22-1994
(1)
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11-23-1970
(1)
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(1)
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11-23-1993
(1)
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11-24-1924
(1)
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11-24-1999
(4)
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11-25-1933
(1)
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(1)
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(3)
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(13)
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(6)
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11-26-1956
(1)
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11-26-1986
(1)
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(8)
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11-26-2002
(2)
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11-27-1942
(1)
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11-27-1959
(2)
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11-27-1995
(2)
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11-27-1998
(1)
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11-28-1930
(1)
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(2)
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(3)
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11-29-1961
(1)
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(1)
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(1)
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11-30-1992
(1)
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(4)
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11-30-1995
(2)
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11-30-2001
(2)
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11/08/1995
(2)
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11/17/08
(2)
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11/26/08
(10)
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11/3/08
(1)
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11/30/08
(1)
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11/5/08
(5)
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1145
(23)
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11th Century
(1)
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11th century
(1)
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12 Dec 1953
(1)
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12 February 196
(1)
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12 Jul 1994
(1)
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12 June 1980
(4)
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12 October 1977
(2)
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12 October 1994
(6)
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12 September 19
(2)
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12-01-1927
(1)
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12-01-1938
(1)
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12-01-1939
(5)
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(1)
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12-01-1964
(1)
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12-01-1984
(17)
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12-01-1990
(2)
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12-01-1994
(2)
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12-01-1996
(7)
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12-01-1997
(1)
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12-01-1998
(12)
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12-01-1999
(5)
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12-02-1937
(1)
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(1)
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12-02-1964
(1)
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12-02-1965
(1)
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(1)
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(1)
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(3)
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(1)
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(1)
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12-03-1963
(1)
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(1)
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12-03-1997
(29)
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12-04-1925
(1)
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12-04-1989
(1)
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(1)
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(2)
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(1)
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(1)
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(1)
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(1)
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(1)
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(1)
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(1)
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(1)
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(1)
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(4)
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(1)
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(1)
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(4)
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(1)
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(5)
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(1)
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(1)
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(1)
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(3)
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(2)
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12-11-1941
(1)
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(1)
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(1)
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12-11-1998
(14)
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(1)
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(5)
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(3)
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12-12-1953
(1)
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(1)
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(1)
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(1)
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(2)
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(1)
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(1)
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(3)
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12-16-1946
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12-17-1926
(2)
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12-17-1997
(7)
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12-17-2000
(2)
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12-18-1942
(1)
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12-18-1944
(1)
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(1)
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(1)
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(1)
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(4)
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12-20-1921
(1)
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(1)
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(10)
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(2)
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12-22-1992
(1)
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(1)
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12-23-1986
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(1)
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(1)
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(1)
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(1)
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12-31-1931
(2)
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12-31-1942
(5)
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(1)
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(3)
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(4)
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12/8/08
(2)
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1200
(8)
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13 April 1960
(4)
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13 March 1964
(1)
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13 Nov 1995
(3)
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14 Apr 1998
(1)
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14 December 196
(2)
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14 June 1991
(2)
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14 Mar 1996
(1)
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14 May 1998
(1)
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14 November 194
(6)
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14 November 199
(4)
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14 October 1947
(1)
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14th Century
(2)
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15 Aug 1963
(1)
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15 Aug 1994
(1)
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15 Feb 1996
(6)
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15 Mar 1963
(1)
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15 Nov 1949
(1)
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15 November 19
(68)
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16 Apr 1999
(4)
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(1)
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(2)
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(3)
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16 July 1971
(2)
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(4)
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16 May 1992
(5)
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16th century
(1)
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(1)
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(1)
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(2)
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17 Jun 1998
(10)
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1733
(1)
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1776
(1)
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(1)
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(4)
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(2)
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(1)
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1824
(1)
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1830
(1)
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1850
(9)
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(2)
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19 March 1956
(3)
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(2)
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19 May 2000
(1)
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19 Nov 1996
(1)
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1903
(8)
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1911
(1)
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1915
(3)
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1916
(1)
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1918
(3)
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1919
(6)
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1920
(7)
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1921
(19)
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1922
(25)
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1923
(17)
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1924
(16)
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1925
(15)
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1926
(24)
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1927
(29)
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1928
(51)
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1929
(65)
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1930
(58)
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1931
(41)
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1932
(17)
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1933
(19)
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1934
(29)
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1935
(13)
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1936
(51)
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1937
(20)
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1938
(51)
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1939
(76)
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1940
(77)
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1941
(69)
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1942
(38)
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1943
(48)
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1944
(32)
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1945
(66)
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1946
(97)
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1947
(83)
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1948
(40)
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1949
(73)
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1950
(63)
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1951
(63)
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1952
(119)
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1953
(103)
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1954
(127)
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1955
(117)
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1956
(72)
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1957
(57)
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1958
(93)
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1959
(241)
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1960
(92)
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1961
(96)
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1962
(201)
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1963
(182)
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1964
(118)
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1965
(69)
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1966
(203)
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1967
(186)
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1968
(99)
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1969
(201)
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1970
(88)
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1971
(87)
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1972
(55)
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1973
(80)
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1974
(98)
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1975
(106)
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1976
(105)
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1977
(81)
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1978
(42)
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1979
(122)
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1980
(75)
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1981
(189)
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1982
(65)
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1983
(100)
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1984
(112)
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1985
(79)
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1986
(44)
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1987
(36)
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1988
(52)
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1989
(79)
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1990
(796)
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1991
(125)
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1992
(172)
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1993
(174)
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1994
(174)
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1995
(306)
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1996
(463)
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1997
(611)
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1998
(694)
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1999
(729)
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19th century
(2)
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19th Century
(1)
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2-11-1985
(1)
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2-12-1969
(1)
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2-13-1973
(1)
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2-15-1958
(1)
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(1)
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2-5-2001
(13)
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2-51-92
(1)
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2-6-1964
(1)
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(17)
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2/19/09
(1)
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2/2/09
(1)
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2/25/09
(1)
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(1)
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20 December 196
(3)
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(2)
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20 July 1951
(2)
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20 July 1955
(6)
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20 November 19
(11)
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20 September 19
(1)
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2000
(713)
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2001
(904)
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2002
(510)
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2003
(205)
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2004
(263)
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2005
(180)
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2006
(165)
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2007
(168)
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2008
(796)
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2009
(570)
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2010
(11)
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20th century
(9)
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21 February 200
(1)
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21 January 2003
(1)
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21 June 1967
(1)
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21 November 195
(6)
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21st Century
(18)
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21st century
(7)
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22 August 1997
(1)
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22 December 197
(2)
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22 June 2007
(7)
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22 May 1956
(1)
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(1)
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2200
(1)
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23 August 1966
(2)
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23 Jul 1979
(1)
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23 June 2007
(1)
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(1)
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24 Jun 2002
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24 June 1971
(8)
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24 May 1972
(1)
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24 October 2000
(1)
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2450
(2)
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25 Apr 1969
(1)
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(4)
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(1)
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25 June 2007
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26 December 200
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(1)
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(1)
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(1)
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27 Aug 1993
(1)
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27 March 2004
(1)
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27 September 19
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28 Jun 1976
(1)
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28 September 19
(3)
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29 April 1948
(1)
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(1)
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30 Apr 1999
(10)
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(1)
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31 March 1996
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31 October 199
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3354
(1)
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3712
(2)
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3723
(5)
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3754
(1)
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4-1-1993
(1)
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4-18-1983
(1)
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(1)
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(1)
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4/2/09
(10)
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(13)
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4/22/09
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(27)
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4/24/09
(1)
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4500
(12)
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5-15-1963
(1)
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(1)
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(1)
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(1)
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5/24/09
(1)
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5000
(1)
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6-1-1926
(1)
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6-11-1991
(1)
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6-27-1973
(1)
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(4)
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(1)
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6/5/08
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(1)
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7-17-1981
(1)
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(1)
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(4)
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(1)
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(2)
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7/1/08
(4)
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7/1/09
(9)
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(1)
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(1)
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7500
(4)
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8-1-1968
(1)
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(1)
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(1)
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(1)
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(1)
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(1)
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(1)
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(1)
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(1)
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(1)
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(4)
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(1)
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(1)
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9/18/09
(1)
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9/23/08
(9)
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9/29/09
(3)
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9/30/08
(2)
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9th Century
(2)
-
Apr 1958
(1)
-
Apr 1997
(1)
-
April 1, 2003
(2)
-
April 10, 1961
(1)
-
April 10, 1996
(1)
-
April 10, 2001
(1)
-
April 11, 1949
(1)
-
April 11, 2004
(1)
-
April 12, 2001
(2)
-
April 12, 2002
(3)
-
April 13, 1967
(1)
-
April 13, 2000
(1)
-
April 13, 2001
(1)
-
April 14, 1969
(2)
-
April 14, 1981
(18)
-
April 14, 1989
(2)
-
April 14, 1998
(1)
-
April 14, 2003
(1)
-
April 14, 2005
(1)
-
April 15, 1959
(1)
-
April 15, 1992
(1)
-
April 16, 1999
(1)
-
April 16, 2001
(1)
-
April 16, 2005
(4)
-
April 17, 1950
(1)
-
April 17, 1969
(31)
-
April 17, 1980
(1)
-
April 17, 1998
(2)
-
April 17, 2001
(1)
-
April 17, 2006
(1)
-
April 18, 1975
(1)
-
April 18, 1978
(2)
-
April 18, 1994
(3)
-
April 18, 1996
(1)
-
April 18, 2004
(8)
-
April 1928
(3)
-
April 1929
(1)
-
April 1935
(4)
-
April 1936
(2)
-
April 1937
(2)
-
April 1939
(1)
-
April 1943
(1)
-
April 1947
(5)
-
April 1948
(2)
-
April 1949
(2)
-
April 1955
(2)
-
April 1959
(2)
-
April 1962
(8)
-
April 1963
(2)
-
April 1964
(18)
-
April 1971
(1)
-
April 1973
(1)
-
April 1975
(2)
-
April 1981
(94)
-
April 1984
(1)
-
April 1987
(3)
-
April 1992
(1)
-
April 1993
(1)
-
April 1994
(6)
-
April 1995
(1)
-
April 1996
(14)
-
April 1997
(4)
-
April 1998
(2)
-
April 1999
(15)
-
April 2, 1985
(1)
-
April 2, 1998
(1)
-
April 2, 2002
(2)
-
April 2, 2003
(1)
-
April 20 1972
(4)
-
April 20, 1951
(1)
-
April 20, 2005
(5)
-
April 2000
(1)
-
April 2001
(5)
-
April 2003
(8)
-
April 2004
(2)
-
April 2005
(4)
-
April 21, 1954
(1)
-
April 21, 2005
(2)
-
April 22, 1949
(1)
-
April 22, 1966
(1)
-
April 22, 1996
(3)
-
April 22, 2003
(2)
-
April 22, 2005
(2)
-
April 23, 1979
(3)
-
April 23, 2003
(1)
-
April 24, 1941
(1)
-
April 24, 1996
(6)
-
April 24, 2001
(2)
-
April 25, 1956
(1)
-
April 25, 1969
(3)
-
April 25, 2001
(2)
-
April 25, 2007
(2)
-
April 26, 1965
(1)
-
April 26, 1968
(1)
-
April 26, 1995
(1)
-
April 26, 2007
(9)
-
April 27, 1953
(1)
-
April 27, 1954
(1)
-
April 27, 1971
(2)
-
April 27, 1975
(3)
-
April 27, 1984
(5)
-
April 28, 1976
(1)
-
April 28, 1978
(1)
-
April 28, 1981
(2)
-
April 28, 2001
(9)
-
April 28, 2002
(1)
-
April 28, 2005
(1)
-
April 28,2001
(1)
-
April 29, 1955
(4)
-
April 29, 1960
(2)
-
April 29, 1990
(1)
-
April 29, 1993
(34)
-
April 3, 1952
(1)
-
April 3, 1958
(1)
-
April 3, 1981
(1)
-
April 3, 1987
(1)
-
April 3, 1998
(1)
-
April 3, 2003
(1)
-
April 30, 1997
(1)
-
April 30, 1999
(7)
-
April 30, 2005
(1)
-
April 4, 2001
(1)
-
April 5, 1963
(2)
-
April 5, 2004
(1)
-
April 7, 1966
(1)
-
April 7, 1980
(1)
-
April 7, 2001
(1)
-
April 8, 2002
(1)
-
April 8, 2003
(1)
-
April 9, 1953
(3)
-
April 9, 1958
(2)
-
April 9, 1959
(1)
-
April, 1929
(1)
-
April, 1980
(3)
-
April, 1981
(5)
-
April, 2003
(2)
-
Aug 1953
(1)
-
Aug 1963
(1)
-
Aug 1995
(2)
-
Aug 1997
(5)
-
August 1, 1927
(2)
-
August 1, 1954
(2)
-
August 1, 1966
(2)
-
August 1, 1973
(8)
-
August 1, 1999
(2)
-
August 1, 2001
(1)
-
August 1, 2002
(2)
-
August 10, 1956
(2)
-
August 10, 1965
(2)
-
August 10, 1966
(1)
-
August 10, 1971
(1)
-
August 10, 2000
(2)
-
August 10, 2006
(4)
-
August 11, 1963
(1)
-
August 11, 1995
(2)
-
August 11, 2005
(2)
-
August 12, 1955
(1)
-
August 12, 197
(10)
-
August 12, 2003
(1)
-
August 12, 2005
(6)
-
August 13, 1977
(1)
-
August 13, 2001
(3)
-
August 13, 2004
(1)
-
August 14, 1952
(1)
-
August 14, 2005
(5)
-
August 14, 2007
(3)
-
August 15, 195
(12)
-
August 15, 1957
(4)
-
August 15, 2005
(1)
-
August 16, 1963
(4)
-
August 16, 1966
(2)
-
August 16, 2000
(1)
-
August 16, 2002
(4)
-
August 16, 2005
(1)
-
August 16, 2006
(1)
-
August 16, 2007
(1)
-
August 16,2001
(1)
-
August 17, 2005
(1)
-
August 18, 1950
(1)
-
August 18, 1964
(1)
-
August 18, 2005
(2)
-
August 19, 1958
(1)
-
August 19, 1963
(1)
-
August 19, 2005
(9)
-
August 1922
(1)
-
August 1924
(1)
-
August 1927
(3)
-
August 1929
(1)
-
August 1942
(2)
-
August 1947
(1)
-
August 1950
(3)
-
August 1954
(1)
-
August 1955
(6)
-
August 1956
(2)
-
August 1959
(1)
-
August 1962
(1)
-
August 1963
(1)
-
August 1965
(1)
-
August 1971
(1)
-
August 1973
(1)
-
August 1974
(2)
-
August 1977
(1)
-
August 1978
(1)
-
August 1982
(2)
-
August 1992
(1)
-
August 1993
(4)
-
August 1994
(2)
-
August 1995
(3)
-
August 1996
(9)
-
August 1997
(3)
-
August 1998
(5)
-
August 1999
(2)
-
August 2, 1976
(1)
-
August 2, 1990
(2)
-
August 2, 1994
(1)
-
August 2, 2001
(1)
-
August 2, 2003
(1)
-
August 20, 1959
(5)
-
August 20, 1975
(1)
-
August 20, 1976
(1)
-
August 20, 1998
(1)
-
August 2000
(2)
-
August 2001
(4)
-
August 2002
(1)
-
August 2005
(6)
-
August 21, 195
(12)
-
August 21, 1959
(2)
-
August 21, 1978
(1)
-
August 21, 2000
(1)
-
August 21, 2001
(1)
-
August 22, 1951
(4)
-
August 22, 1963
(5)
-
August 22, 1997
(1)
-
August 22, 2002
(3)
-
August 23, 2005
(1)
-
August 24, 1962
(1)
-
August 24, 2006
(4)
-
August 25, 1999
(2)
-
August 25, 2003
(5)
-
August 25, 2007
(7)
-
August 26, 1954
(6)
-
August 26, 2000
(1)
-
August 26, 2002
(1)
-
August 26, 2006
(1)
-
August 27, 1951
(2)
-
August 27, 1956
(1)
-
August 27, 2003
(7)
-
August 28, 195
(12)
-
August 28, 1964
(2)
-
August 29, 1995
(3)
-
August 30, 1963
(1)
-
August 30, 1982
(1)
-
August 30, 2005
(2)
-
August 31, 1951
(3)
-
August 31, 1956
(1)
-
August 31, 1971
(2)
-
August 31, 2005
(9)
-
August 4, 1949
(1)
-
August 4, 1953
(2)
-
August 4, 1967
(1)
-
August 5 1954
(1)
-
August 5, 1930
(1)
-
August 5, 1963
(1)
-
August 6, 1985
(2)
-
August 6, 1993
(3)
-
August 7, 1951
(12)
-
August 7, 1961
(1)
-
August 7, 1980
(1)
-
August 7, 1982
(10)
-
August 8, 1955
(10)
-
August 8, 1993
(2)
-
August 9, 1970
(1)
-
August 9, 2005
(34)
-
August 9, 2007
(4)
-
August, 1995
(2)
-
August, 1997
(5)
-
Dec 1990
(1)
-
Dec 1994
(1)
-
Dec 1996
(2)
-
December 1, 19
(15)
-
December 1, 198
(6)
-
December 1, 199
(1)
-
December 1,1985
(1)
-
December 10, 19
(4)
-
December 11, 20
(4)
-
December 11, 20
(1)
-
December 12, 19
(1)
-
December 12, 19
(5)
-
December 12, 19
(4)
-
December 12, 19
(1)
-
December 12, 20
(1)
-
December 13, 19
(5)
-
December 13, 19
(1)
-
December 13, 20
(4)
-
December 14, 19
(1)
-
December 15, 19
(2)
-
December 15, 19
(1)
-
December 15, 20
(5)
-
December 16, 19
(1)
-
December 16, 1
(12)
-
December 16, 19
(3)
-
December 16, 20
(1)
-
December 17, 19
(3)
-
December 17, 19
(1)
-
December 17, 20
(1)
-
December 17, 2
(18)
-
December 18, 19
(1)
-
December 19, 19
(4)
-
December 19, 19
(9)
-
December 19, 20
(6)
-
December 1903
(1)
-
December 1926
(1)
-
December 1928
(1)
-
December 1929
(3)
-
December 1930
(1)
-
December 1939
(1)
-
December 1941
(1)
-
December 1942
(3)
-
December 1944
(1)
-
December 1946
(42)
-
December 1947
(1)
-
December 1948
(1)
-
December 1952
(2)
-
December 1954
(11)
-
December 1955
(3)
-
December 1959
(1)
-
December 1960
(8)
-
December 1961
(5)
-
December 1963
(5)
-
December 1965
(1)
-
December 1966
(19)
-
December 1967
(2)
-
December 1968
(2)
-
December 1969
(73)
-
December 1973
(15)
-
December 1975
(1)
-
December 1984
(2)
-
December 1985
(3)
-
December 1987
(2)
-
December 1988
(4)
-
December 1990
(3)
-
December 1991
(3)
-
December 1993
(34)
-
December 1994
(1)
-
December 1995
(5)
-
December 1996
(99)
-
December 1997
(11)
-
December 1998
(26)
-
December 1999
(18)
-
December 1st, 1
(9)
-
December 2, 194
(1)
-
December 2, 196
(2)
-
December 2, 196
(1)
-
December 2, 199
(1)
-
December 20, 1
(12)
-
December 20, 19
(4)
-
December 20, 19
(8)
-
December 20, 19
(1)
-
December 20, 19
(1)
-
December 20, 19
(7)
-
December 2000
(7)
-
December 2001
(7)
-
December 2002
(3)
-
December 2003
(2)
-
December 2004
(5)
-
December 21, 19
(2)
-
December 21, 19
(6)
-
December 21, 1
(10)
-
December 21, 19
(1)
-
December 21, 19
(9)
-
December 22, 19
(1)
-
December 22, 1
(11)
-
December 22, 19
(1)
-
December 22, 20
(1)
-
December 23, 20
(1)
-
December 24, 19
(9)
-
December 26, 19
(9)
-
December 26, 20
(1)
-
December 27, 20
(1)
-
December 29, 19
(1)
-
December 29, 20
(2)
-
December 3, 196
(1)
-
December 3, 199
(1)
-
December 3, 19
(10)
-
December 30, 20
(1)
-
December 31, 20
(2)
-
December 4, 200
(2)
-
December 4, 200
(5)
-
December 5, 200
(1)
-
December 6, 195
(1)
-
December 6, 199
(1)
-
December 6, 200
(1)
-
December 7, 200
(1)
-
December 8, 190
(1)
-
December 8, 192
(3)
-
December 8, 195
(2)
-
December 9, 194
(3)
-
December 9, 196
(2)
-
December 9, 196
(2)
-
December 9, 200
(1)
-
December 9, 200
(1)
-
December 9, 200
(1)
-
December, 1930
(3)
-
December, 1941
(2)
-
December, 1960
(1)
-
Feb 1990
(1)
-
Feb 1994
(1)
-
Feb 1995
(1)
-
Feb 1999
(1)
-
February 1, 196
(2)
-
February 11, 19
(2)
-
February 11, 20
(1)
-
February 12, 19
(5)
-
February 12, 19
(1)
-
February 12, 19
(1)
-
February 13, 19
(2)
-
February 13, 19
(1)
-
February 13, 20
(1)
-
February 13, 20
(2)
-
February 14, 20
(1)
-
February 14, 20
(1)
-
February 15, 19
(1)
-
February 16, 20
(4)
-
February 17, 20
(1)
-
February 18, 19
(7)
-
February 18, 19
(1)
-
February 1925
(2)
-
February 1928
(2)
-
February 1929
(2)
-
February 1931
(1)
-
February 1941
(2)
-
February 1948
(2)
-
February 1953
(2)
-
February 1960
(2)
-
February 1962
(5)
-
February 1963
(1)
-
February 1964
(3)
-
February 1971
(1)
-
February 1977
(2)
-
February 1986
(3)
-
February 1992
(46)
-
February 1994
(1)
-
February 1996
(4)
-
February 1997
(2)
-
February 1998
(19)
-
February 1999
(8)
-
February 2, 199
(1)
-
February 2, 200
(1)
-
February 2, 200
(2)
-
February 2, 200
(1)
-
February 20, 19
(3)
-
February 20, 19
(5)
-
February 20, 19
(2)
-
February 20, 19
(1)
-
February 20, 19
(2)
-
February 20, 20
(8)
-
February 2001
(20)
-
February 2002
(2)
-
February 2003
(1)
-
February 2004
(3)
-
February 2005
(2)
-
February 2007
(8)
-
February 21, 19
(2)
-
February 21, 19
(1)
-
February 21, 20
(3)
-
February 21, 20
(5)
-
February 23, 20
(1)
-
February 24 200
(1)
-
February 24, 19
(1)
-
February 24, 19
(1)
-
February 24, 20
(1)
-
February 24, 20
(4)
-
February 25, 19
(1)
-
February 25, 19
(5)
-
February 26, 19
(1)
-
February 26, 2
(11)
-
February 27, 19
(6)
-
February 28, 19
(1)
-
February 3, 192
(2)
-
February 3, 196
(1)
-
February 3, 199
(2)
-
February 3, 200
(1)
-
February 4, 19
(12)
-
February 4, 197
(1)
-
February 4, 199
(2)
-
February 4, 200
(1)
-
February 5, 195
(1)
-
February 5, 197
(1)
-
February 5, 199
(1)
-
February 5, 199
(2)
-
February 6, 195
(2)
-
February 6, 199
(2)
-
February 6, 199
(9)
-
February 7, 196
(2)
-
February 7, 198
(2)
-
February 7, 200
(3)
-
February 7, 200
(1)
-
February 8, 197
(1)
-
February 8, 200
(1)
-
February 8,1951
(3)
-
February 9, 192
(2)
-
February 9, 200
(1)
-
first century
(10)
-
January 10, 197
(4)
-
January 11, 195
(1)
-
January 11, 196
(1)
-
January 12, 199
(6)
-
January 12, 200
(1)
-
January 12, 200
(2)
-
January 13, 200
(2)
-
January 14, 199
(1)
-
January 16, 200
(1)
-
January 17, 199
(2)
-
January 17, 200
(9)
-
January 18, 200
(1)
-
January 18, 200
(1)
-
January 19, 199
(1)
-
January 19, 199
(4)
-
January 1925
(1)
-
January 1927
(2)
-
January 1933
(1)
-
January 1939
(1)
-
January 1944
(2)
-
January 1948
(2)
-
January 1950
(2)
-
January 1952
(3)
-
January 1957
(1)
-
January 1958
(2)
-
January 1959
(1)
-
January 1962
(1)
-
January 1964
(1)
-
January 1966
(43)
-
January 1967
(20)
-
January 1971
(3)
-
January 1975
(1)
-
January 1976
(1)
-
January 1977
(2)
-
January 1983
(4)
-
January 1986
(1)
-
January 1987
(4)
-
January 1988
(4)
-
January 1990
(2)
-
January 1992
(1)
-
January 1994
(3)
-
January 1996
(4)
-
January 1997
(4)
-
January 2, 1966
(1)
-
January 20, 196
(2)
-
January 2000
(23)
-
January 2001
(1)
-
January 2002
(4)
-
January 2003
(1)
-
January 2004
(3)
-
January 22, 198
(2)
-
January 22, 200
(2)
-
January 22, 200
(2)
-
January 22, 200
(1)
-
January 23, 195
(1)
-
January 24, 200
(1)
-
January 24, 200
(2)
-
January 25, 19
(19)
-
January 26, 199
(1)
-
January 26, 200
(2)
-
January 26, 200
(5)
-
January 26, 200
(1)
-
January 27, 195
(2)
-
January 27, 195
(1)
-
January 27, 19
(12)
-
January 28, 197
(2)
-
January 28, 199
(3)
-
January 28, 199
(2)
-
January 29, 197
(1)
-
January 3, 1925
(1)
-
January 3, 2002
(1)
-
January 30, 196
(1)
-
January 30, 199
(2)
-
January 31, 200
(3)
-
January 31, 200
(3)
-
January 31, 200
(1)
-
January 4, 1999
(1)
-
January 7, 1953
(5)
-
January 7, 1959
(2)
-
January 8, 1992
(1)
-
January 8, 1997
(1)
-
January 9, 1952
(2)
-
January 9, 1963
(3)
-
January 9, 1999
(2)
-
January 9, 2001
(9)
-
January, 1953
(2)
-
Jul 1996
(1)
-
Jul 1998
(1)
-
July 1, 1954
(2)
-
July 1, 1959
(1)
-
July 1, 1960
(1)
-
July 1, 1966
(2)
-
July 1, 1980
(1)
-
July 1, 2007
(5)
-
July 10, 1993
(2)
-
July 10, 2001
(5)
-
July 10, 2002
(6)
-
July 11, 1952
(3)
-
July 11, 1994
(1)
-
July 11, 2000
(5)
-
July 11, 2004
(1)
-
July 11, 2006
(1)
-
July 12, 1951
(1)
-
July 12, 1966
(20)
-
July 12, 1993
(2)
-
July 12, 2000
(2)
-
July 13, 2006
(4)
-
July 14, 1954
(1)
-
July 14, 1976
(4)
-
July 14, 2001
(8)
-
July 14, 2004
(2)
-
July 15, 1975
(2)
-
July 15, 1981
(1)
-
July 15, 2003
(1)
-
July 16, 1962
(1)
-
July 16, 1997
(1)
-
July 17, 1933
(2)
-
July 17, 1963
(1)
-
July 17, 1970
(12)
-
July 17, 1997
(1)
-
July 17, 2000
(1)
-
July 17, 2001
(1)
-
July 18, 2001
(1)
-
July 18, 2002
(1)
-
July 19, 1984
(1)
-
July 19, 2003
(1)
-
July 1922
(1)
-
July 1932
(1)
-
July 1942
(5)
-
July 1944
(3)
-
July 1945
(3)
-
July 1947
(1)
-
July 1951
(2)
-
July 1952
(2)
-
July 1954
(8)
-
July 1955
(5)
-
July 1958
(2)
-
July 1959
(4)
-
July 1962
(8)
-
July 1966
(35)
-
July 1969
(6)
-
July 1973
(2)
-
July 1982
(2)
-
July 1987
(1)
-
July 1988
(3)
-
July 1991
(4)
-
July 1994
(1)
-
July 1995
(2)
-
July 1996
(7)
-
July 1997
(8)
-
July 1998
(6)
-
July 1999
(8)
-
July 2, 1980
(1)
-
July 2, 1996
(5)
-
July 20, 1951
(4)
-
July 20, 1955
(6)
-
July 20, 1969
(13)
-
July 20, 1976
(1)
-
July 20, 2000
(8)
-
July 20, 2005
(1)
-
July 20, 2007
(3)
-
July 20,1969
(3)
-
July 2001
(2)
-
July 2002
(11)
-
July 2003
(1)
-
July 2004
(2)
-
July 21, 2004
(1)
-
July 22, 2001
(1)
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July 22, 2005
(3)
-
July 24, 1951
(2)
-
July 24, 1991
(1)
-
July 24, 2000
(8)
-
July 25, 1958
(4)
-
July 25, 1967
(1)
-
July 25, 1991
(1)
-
July 25, 2001
(2)
-
July 26, 1958
(1)
-
July 26, 1977
(2)
-
July 26, 1999
(1)
-
July 26, 2005
(1)
-
July 27, 1995
(2)
-
July 27, 2001
(1)
-
July 27, 2006
(3)
-
July 28, 1977
(1)
-
July 28, 1981
(2)
-
July 28, 1982
(1)
-
July 28, 1994
(1)
-
July 28, 2000
(1)
-
July 29, 1940
(1)
-
July 29, 1950
(1)
-
July 29, 1985
(2)
-
July 3, 1986
(2)
-
July 30, 1919
(1)
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July 30, 1958
(2)
-
July 30, 1971
(2)
-
July 30, 2001
(6)
-
July 30, 2003
(10)
-
July 31, 1950
(1)
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July 31, 1990
(1)
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July 31, 1996
(1)
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July 31, 2001
(1)
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July 31, 2002
(1)
-
July 4, 1776
(1)
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July 4, 1982
(4)
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July 5, 1982
(6)
-
July 6, 2005
(1)
-
July 6, 2006
(1)
-
July 7, 1955
(1)
-
July 7, 1997
(40)
-
July 9, 1980
(1)
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July 9, 1999
(2)
-
July 9, 2000
(1)
-
July, 1962
(1)
-
July, 1977
(1)
-
July, 1995
(1)
-
July, 2002
(16)
-
July, 2004
(1)
-
June 1, 1942
(2)
-
June 1, 1983
(8)
-
June 1, 2001
(1)
-
June 1, 2004
(3)
-
June 10, 1977
(1)
-
June 10, 2002
(1)
-
June 11, 1955
(50)
-
June 11, 1998
(1)
-
June 11, 2000
(3)
-
June 11, 2003
(1)
-
June 12, 1979
(3)
-
June 12, 1980
(9)
-
June 12, 2002
(1)
-
June 12, 2006
(1)
-
June 13, 1966
(2)
-
June 14, 1978
(1)
-
June 15, 1932
(1)
-
June 15, 1961
(1)
-
June 15, 1991
(2)
-
June 15, 1993
(3)
-
June 15, 2004
(2)
-
June 16, 1956
(1)
-
June 16, 1972
(1)
-
June 16, 1980
(1)
-
June 16, 2001
(1)
-
June 16, 2002
(1)
-
June 16, 2004
(1)
-
June 17, 2000
(1)
-
June 17, 2003
(4)
-
June 18, 1956
(3)
-
June 18, 1971
(1)
-
June 18, 1978
(1)
-
June 18, 1982
(1)
-
June 18, 2003
(1)
-
June 19, 1961
(1)
-
June 19, 2001
(1)
-
June 19, 2002
(2)
-
June 1920
(1)
-
June 1921
(1)
-
June 1922
(1)
-
June 1933
(4)
-
June 1940
(1)
-
June 1941
(3)
-
June 1943
(2)
-
June 1947
(1)
-
June 1950
(1)
-
June 1953
(1)
-
June 1954
(14)
-
June 1956
(1)
-
June 1957
(6)
-
June 1959
(124)
-
June 1962
(2)
-
June 1963
(3)
-
June 1966
(1)
-
June 1967
(9)
-
June 1969
(8)
-
June 1971
(1)
-
June 1975
(1)
-
June 1977
(7)
-
June 1983
(1)
-
June 1991
(2)
-
June 1993
(1)
-
June 1995
(14)
-
June 1996
(16)
-
June 1997
(18)
-
June 1998
(4)
-
June 1999
(28)
-
June 2, 1970
(11)
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June 2, 2001
(10)
-
June 2, 2005
(2)
-
June 20, 1952
(2)
-
June 20, 2001
(1)
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June 20, 2005
(5)
-
June 2000
(1)
-
June 2001
(2)
-
June 2002
(5)
-
June 2003
(1)
-
June 2004
(12)
-
June 2005
(1)
-
June 21, 1985
(2)
-
June 21, 2000
(1)
-
June 22, 1977
(1)
-
June 22, 2000
(5)
-
June 22, 2004
(5)
-
June 22, 2007
(22)
-
June 23, 1954
(1)
-
June 23, 2007
(10)
-
June 25, 1995
(4)
-
June 25, 2003
(1)
-
June 25, 2007
(1)
-
June 26, 1929
(12)
-
June 26, 1953
(4)
-
June 26, 1959
(1)
-
June 27, 1945
(2)
-
June 27, 1962
(3)
-
June 27, 1963
(2)
-
June 27, 1975
(1)
-
June 27, 1997
(1)
-
June 27, 1998
(25)
-
June 27, 2007
(3)
-
June 28, 1963
(1)
-
June 28, 2001
(1)
-
June 28, 2007
(2)
-
June 29, 1951
(4)
-
June 29, 1998
(2)
-
June 29, 1999
(3)
-
June 29, 2004
(1)
-
June 3, 1999
(4)
-
June 30, 2001
(2)
-
June 30, 2003
(3)
-
June 4, 1954
(1)
-
June 4, 1971
(8)
-
June 4, 1997
(15)
-
June 4, 2001
(1)
-
June 5, 1916
(1)
-
June 5, 1949
(2)
-
June 5, 1978
(2)
-
June 6, 1967
(1)
-
June 6, 1969
(1)
-
June 6, 2001
(1)
-
June 7, 2001
(1)
-
June 7, 2003
(2)
-
June 8, 1944
(2)
-
June 8, 1959
(1)
-
June 8, 1966
(17)
-
June 8, 1978
(1)
-
June 8, 2007
(15)
-
June 9, 1997
(2)
-
June 9, 2002
(1)
-
June 9, 2003
(12)
-
June, 1940
(1)
-
June, 1950
(1)
-
June, 2004
(16)
-
Mar 1991
(1)
-
Mar 1996
(1)
-
Mar 1997
(11)
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Mar 1998
(1)
-
Mar 2000
(2)
-
March 1, 1962
(1)
-
March 1, 1976
(2)
-
March 1, 1994
(1)
-
March 1, 2000
(20)
-
March 1, 2001
(13)
-
March 10, 1948
(5)
-
March 10, 1979
(1)
-
March 10, 2004
(8)
-
March 11, 1945
(1)
-
March 11, 1959
(1)
-
March 11, 1964
(1)
-
March 11, 1999
(1)
-
March 11, 2002
(1)
-
March 11, 2004
(10)
-
March 12, 1962
(2)
-
March 12, 1980
(2)
-
March 12, 199
(100)
-
March 12, 2001
(1)
-
March 12, 2004
(1)
-
March 13, 1964
(1)
-
March 13, 1978
(1)
-
March 13, 2001
(1)
-
March 13, 2002
(1)
-
March 13, 2004
(8)
-
March 14, 1979
(2)
-
March 14, 1980
(1)
-
March 14, 1988
(3)
-
March 14, 1991
(2)
-
March 14, 2000
(1)
-
March 14, 2001
(4)
-
March 15, 1929
(1)
-
March 15, 1968
(2)
-
March 15, 1994
(2)
-
March 15, 2001
(5)
-
March 15, 2002
(1)
-
March 16, 2004
(7)
-
March 16, 2007
(1)
-
March 17, 1953
(1)
-
March 17, 1971
(1)
-
March 17, 1993
(2)
-
March 17, 1996
(3)
-
March 17, 2004
(5)
-
March 17, 2005
(1)
-
March 18, 1952
(1)
-
March 18, 1995
(1)
-
March 18, 1998
(1)
-
March 19, 1956
(6)
-
March 19, 1964
(1)
-
March 19, 1970
(30)
-
March 19, 2001
(1)
-
March 19, 2004
(1)
-
March 1915
(1)
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March 1929
(1)
-
March 1934
(1)
-
March 1935
(1)
-
March 1941
(1)
-
March 1943
(3)
-
March 1944
(2)
-
March 1945
(6)
-
March 1951
(1)
-
March 1962
(1)
-
March 1963
(2)
-
March 1966
(8)
-
March 1967
(6)
-
March 1976
(4)
-
March 1979
(10)
-
March 1985
(6)
-
March 1988
(2)
-
March 1990
(4)
-
March 1991
(1)
-
March 1993
(42)
-
March 1994
(2)
-
March 1995
(2)
-
March 1996
(10)
-
March 1997
(18)
-
March 1998
(14)
-
March 1999
(8)
-
March 2, 1977
(2)
-
March 2, 2003
(2)
-
March 20, 1980
(2)
-
March 2000
(104)
-
March 2001
(42)
-
March 2002
(15)
-
March 2003
(1)
-
March 2004
(84)
-
March 2005
(2)
-
March 2007
(3)
-
March 21, 1963
(1)
-
March 21, 1997
(2)
-
March 21, 2002
(2)
-
March 22, 1954
(1)
-
March 22, 1967
(1)
-
March 22, 1996
(2)
-
March 23, 1950
(1)
-
March 23, 1978
(3)
-
March 23, 1990
(2)
-
March 23, 2002
(1)
-
March 23, 2004
(1)
-
March 24, 1995
(2)
-
March 24, 1998
(4)
-
March 25, 1960
(5)
-
March 25, 1963
(1)
-
March 25, 1999
(1)
-
March 26, 1952
(2)
-
March 26, 1976
(6)
-
March 26, 2001
(1)
-
March 26, 2004
(1)
-
March 27, 1992
(1)
-
March 27, 1996
(6)
-
March 27, 2002
(2)
-
March 27, 2003
(1)
-
March 27, 2004
(16)
-
March 28, 1979
(2)
-
March 28, 2001
(2)
-
March 28, 2003
(1)
-
March 29, 1996
(3)
-
March 29, 2005
(1)
-
March 3, 1978
(1)
-
March 3, 1993
(1)
-
March 3, 1998
(1)
-
March 3, 2003
(1)
-
March 30, 1936
(1)
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March 30, 1952
(2)
-
March 30, 1961
(1)
-
March 30, 2004
(2)
-
March 31, 1960
(3)
-
March 31, 1996
(2)
-
March 31, 2004
(1)
-
March 4, 1998
(5)
-
March 4, 2001
(1)
-
March 5, 1999
(3)
-
March 5, 2007
(17)
-
March 6, 1967
(1)
-
March 6, 2000
(1)
-
March 6, 2001
(1)
-
March 6, 2007
(2)
-
March 7, 1979
(2)
-
March 7, 2002
(1)
-
March 8, 1995
(1)
-
March 8, 2001
(1)
-
March 8, 2004
(3)
-
March 9, 1971
(10)
-
March 9, 1979
(2)
-
March 9, 2001
(1)
-
March 9, 2005
(1)
-
March 9, 2007
(1)
-
March, 2001
(1)
-
March, 2002
(11)
-
March, 2005
(19)
-
May 1, 1965
(6)
-
May 1, 1996
(3)
-
May 1, 2001
(9)
-
May 1, 2006
(1)
-
May 1,2002
(1)
-
May 10, 1951
(4)
-
May 10, 1967
(21)
-
May 10, 2007
(5)
-
May 11, 1965
(1)
-
May 12, 1953
(2)
-
May 12, 1955
(1)
-
May 12, 2001
(1)
-
May 13, 2001
(1)
-
May 14, 2002
(1)
-
May 15, 1963
(3)
-
May 15, 1997
(1)
-
May 16 1992
(1)
-
May 16, 1992
(1)
-
May 16, 2006
(1)
-
May 17, 1974
(1)
-
May 17, 1976
(1)
-
May 17, 1978
(1)
-
May 17, 1997
(25)
-
May 18, 1995
(4)
-
May 19, 1936
(2)
-
May 19, 1970
(1)
-
May 19, 2001
(1)
-
May 1926
(1)
-
May 1930
(4)
-
May 1936
(2)
-
May 1943
(2)
-
May 1945
(1)
-
May 1948
(1)
-
May 1951
(2)
-
May 1952
(1)
-
May 1953
(1)
-
May 1956
(1)
-
May 1957
(1)
-
May 1960
(1)
-
May 1961
(1)
-
May 1965
(2)
-
May 1967
(2)
-
May 1968
(2)
-
May 1970
(4)
-
May 1983
(2)
-
May 1989
(1)
-
May 1992
(2)
-
May 1996
(2)
-
May 1997
(7)
-
May 1998
(3)
-
May 1999
(2)
-
May 2, 2002
(1)
-
May 2, 2007
(1)
-
May 20, 1938
(1)
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May 20, 1969
(1)
-
May 20, 2001
(1)
-
May 20, 2003
(1)
-
May 2000
(8)
-
May 2001
(4)
-
May 2007
(1)
-
May 21, 1981
(4)
-
May 21, 1993
(1)
-
May 21, 1997
(1)
-
May 21, 2004
(1)
-
May 22, 1975
(7)
-
May 22, 1992
(1)
-
May 22, 1995
(5)
-
May 22, 2001
(1)
-
May 22, 2002
(4)
-
May 23, 1934
(1)
-
May 23, 1973
(10)
-
May 23, 1976
(1)
-
May 23, 1989
(2)
-
May 23, 2001
(1)
-
May 24, 1949
(2)
-
May 24, 1950
(1)
-
May 24, 1996
(16)
-
May 24, 2005
(3)
-
May 24, 2007
(1)
-
May 25, 1958
(2)
-
May 25, 1961
(1)
-
May 25, 1962
(3)
-
May 25, 1972
(13)
-
May 25, 2000
(2)
-
May 25, 2001
(23)
-
May 26, 1959
(2)
-
May 26, 2000
(1)
-
May 27, 1931
(5)
-
May 27, 1952
(2)
-
May 27, 1966
(2)
-
May 27, 1992
(1)
-
May 27, 2003
(1)
-
May 27,, 1931
(3)
-
May 28, 2002
(1)
-
May 29, 1996
(6)
-
May 29, 1998
(2)
-
May 3, 1948
(1)
-
May 3, 1998
(2)
-
May 3, 2006
(1)
-
May 3, 2007
(3)
-
May 30, 1996
(2)
-
May 31, 1923
(1)
-
May 31, 1971
(2)
-
May 31, 2007
(12)
-
May 4, 1926
(2)
-
May 4, 1993
(1)
-
May 4, 2001
(1)
-
May 5, 2000
(1)
-
May 5, 2005
(5)
-
May 5, 2006
(3)
-
May 5, 2007
(8)
-
May 6, 1960
(1)
-
May 6, 1974
(1)
-
May 7, 1954
(4)
-
May 7, 1986
(1)
-
May 7, 2001
(2)
-
May 8, 1950
(1)
-
May 8, 1967
(1)
-
May 8, 2001
(3)
-
May 8, 2002
(1)
-
May 9, 1945
(1)
-
May 9, 1969
(12)
-
May 9, 2001
(1)
-
May, 1976
(10)
-
May, 1984
(1)
-
May, 2004
(1)
-
May, 2006
(1)
-
May, 6, 1997
(1)
-
Nov 1951
(1)
-
Nov 1995
(1)
-
Nov 1996
(1)
-
November 1, 198
(1)
-
November 1, 199
(1)
-
November 1, 200
(1)
-
November 10, 19
(1)
-
November 11, 19
(1)
-
November 12, 19
(1)
-
November 12, 19
(1)
-
November 12, 1
(15)
-
November 12, 1
(25)
-
November 12, 20
(1)
-
November 13, 19
(1)
-
November 13, 19
(7)
-
November 13, 19
(1)
-
November 13, 20
(1)
-
November 14, 19
(1)
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November 14, 19
(2)
-
November 14, 19
(1)
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November 14, 19
(2)
-
November 14, 20
(2)
-
November 15, 19
(1)
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November 15, 19
(2)
-
November 15, 19
(1)
-
November 15, 19
(3)
-
November 15, 19
(8)
-
November 15, 20
(2)
-
November 15, 20
(1)
-
November 15, 20
(1)
-
November 16, 19
(1)
-
November 16, 2
(15)
-
November 16, 20
(4)
-
November 17, 19
(2)
-
November 18, 19
(1)
-
November 18, 19
(1)
-
November 18, 20
(2)
-
November 19, 19
(2)
-
November 19, 19
(2)
-
November 19, 19
(1)
-
November 19, 1
(19)
-
November 19, 20
(2)
-
November 1923
(1)
-
November 1928
(3)
-
November 1929
(5)
-
November 1941
(2)
-
November 1946
(1)
-
November 1947
(1)
-
November 1949
(4)
-
November 1950
(13)
-
November 1951
(2)
-
November 1957
(12)
-
November 1959
(2)
-
November 1961
(1)
-
November 1962
(3)
-
November 1964
(1)
-
November 1967
(2)
-
November 1975
(36)
-
November 1977
(1)
-
November 1978
(1)
-
November 1979
(67)
-
November 1981
(3)
-
November 1982
(4)
-
November 1986
(4)
-
November 1987
(1)
-
November 1990
(17)
-
November 1991
(26)
-
November 1993
(5)
-
November 1994
(1)
-
November 1995
(5)
-
November 1996
(9)
-
November 1997
(1)
-
November 1998
(5)
-
November 1999
(8)
-
November 2, 196
(1)
-
November 2, 200
(9)
-
November 20, 1
(19)
-
November 20, 19
(1)
-
November 20, 20
(1)
-
November 2001
(2)
-
November 2002
(2)
-
November 2004
(2)
-
November 2005
(4)
-
November 2006
(8)
-
November 21, 19
(1)
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November 21, 19
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|
Dryden's T-38 Talon Trainer
NASA Dryden's T-38 Talon tra
10/2/08
Description |
NASA Dryden's T-38 Talon trainer jet in flight over the main base complex at Edwards Air Force Base. Formerly at NASA's Langley Research Center, this Northrop T-38 Talon is now used for mission support and pilot proficiency at the Dryden Flight Research Center. May 5, 2006 NASA / photo Jim Ross ED06-0072-2 |
Date |
10/2/08 |
|
NASA Dryden's T-38 Talon Tra
NASA Dryden's T-38 Talon tra
10/2/08
Description |
NASA Dryden's T-38 Talon trainer aircraft in flight near Edwards Air Force Base. Formerly at NASA's Langley Research Center, this Northrop T-38 Talon is now used for mission support and pilot proficiency at the Dryden Flight Research Center. May 5, 2006 NASA / Photo Jim Ross ED06-0072-4 |
Date |
10/2/08 |
|
Northrop T-38 Talon During M
NASA Dryden's T-38 trainer a
10/2/08
Description |
NASA Dryden's T-38 trainer aircraft in flight over Cuddeback Dry Lake in Southern California. Formerly at NASA's Langley Research Center, this Northrop T-38 Talon is now used for mission support and pilot proficiency at the Dryden Flight Research Center. May 5, 2006 NASA / Photo Jim Ross ED06-0072-8 |
Date |
10/2/08 |
|
DC-8
Alternative Jet Fuels Put to
1/29/09
Description |
Alternative Jet Fuels Put to the Test at NASA Dryden ›, Read Feature Bruce Anderson of NASA Langley Research Center and David Liscinsky of United Technologies Research Center tie down sampling lines between the exhaust inlet probe and instrument trailers during synthetic fuel performance and emissions testing at NASA's Dryden Aircraft Operations Facility in Palmdale, Calif. January 22, 2009 NASA Photo / Tom Tschida ED09-0015-01 |
Date |
1/29/09 |
|
DC-8
Alternative Jet Fuels Put to
1/29/09
Description |
Alternative Jet Fuels Put to the Test at NASA Dryden ›, Read Feature Bruce Anderson of NASA Langley Research Center and David Liscinsky of United Technologies Research Center tie down sampling lines between the exhaust inlet probe and instrument trailers during synthetic fuel performance and emissions testing at NASA's Dryden Aircraft Operations Facility in Palmdale, Calif. January 22, 2009 NASA Photo / Tom Tschida ED09-0015-02 |
Date |
1/29/09 |
|
DC-8
Alternative Jet Fuels Put to
1/29/09
Description |
Alternative Jet Fuels Put to the Test at NASA Dryden ›, Read Feature Brad Besheres of the U.S. Army's Arnold Engineering Development Center explains probe arrangement on an engine exhaust sampling rake to project scientist Bruce Anderson of NASA's Langley Research Center during alternative aviation fuels performance and emissions testing at NASA's Dryden Aircraft Operations Facility in Palmdale, Calif. January 22, 2009 NASA Photo / Tom Tschida ED09-0015-07 |
Date |
1/29/09 |
|
DC-8
Alternative Jet Fuels Put to
1/30/09
Description |
Alternative Jet Fuels Put to the Test at NASA Dryden ›, Read Feature Alternatives Aviation Fuels Experiment project scientist Bruce Anderson of NASA's Langley Research Center repairs a malfunctioning instrument shortly before an emissions test during synthetic fuels engine testing at the Dryden Aircraft Operations Facility in Palmdale, Calif. January 27, 2009 NASA Photo / Tom Tschida ED09-0015-75 |
Date |
1/30/09 |
|
DC-8
Alternative Jet Fuels Put to
1/29/09
Description |
Alternative Jet Fuels Put to the Test at NASA Dryden ›, Read Feature NASA Langley's Bruce Anderson and United Technologies' David Liscinsky install tubing to connect pressure ports located on the exhaust inlet probe with sensors located in equipment trailers during synthetic fuel emissions and performance testing at NASA's Dryden Aircraft Operations Facility in Palmdale, Calif. January 22, 2009 NASA Photo / Tom Tschida ED09-0015-04 |
Date |
1/29/09 |
|
Operation Ice Bridge 2009
ED09-0284-2 Operation Ice Br
10/9/09
Description |
ED09-0284-2 Operation Ice Bridge 2009 Glen Sachse of NASA's Langley Research Center adjusts the Differential Absorption CO Measurement, or DACOM, instrument developed at Langley after its installation on NASA's DC-8 flying laboratory. DACOM measures carbon monoxide, nitrous oxide and methane during the Operation Ice Bridge mission to the Antarctic. September 29, 2009 NASA photo / Tom Tschida |
Date |
10/9/09 |
|
DC-8
ED09-0284-8 The Differential
10/8/09
Description |
ED09-0284-8 The Differential Absorption CO Measurement, or DACOM, instrument developed at NASA's Langley Research Center is mounted in NASA's DC-8 flying laboratory in preparation for the Operation Ice Bridge deployment to the Antarctic. Glen Sachse of NASA Langley prepares the DACOM for its air-sampling mission to South America and the Antarctic. September 29, 2009 NASA Photo / Tom Tschida |
Date |
10/8/09 |
|
Operation Ice Bridge 2009
ED09-0284-23 NASA Langley Re
10/9/09
Description |
ED09-0284-23 NASA Langley Research Center researcher Glen Sachse pours liquid nitrogen in a dewar used to keep the infrared detectors of the Differential Absorption CO Measurement instrument cold. Developed at NASA Langley, the instrument is installed on NASA's DC-8 airborne laboratory and will be used to measure carbon monoxide, methane, and nitrous oxide concentrations during the Operation Ice Bridge mission to Antarctica. September 29, 2009 NASA Photo / Tom Tschida |
Date |
10/9/09 |
|
Photo Description |
Formerly at NASA's Langley Research Center, this Northrop T-38 Talon is now used for mission support and pilot proficiency at the Dryden Flight Research Center. |
Project Description |
A sleek, supersonic T-38 trainer jet is taxied into the parking ramp at NASA's Dryden Flight Research Center by Dryden's chief pilot Gordon Fullerton, marking the return of the type to Dryden for the first time in more than 10 years. Formerly assigned to NASA's Langley Research Center in Hampton, Va., the aircraft had supported various aeronautics research projects there for a number of years. The aircraft will be used by NASA Dryden's research pilots for proficiency and mission support flights. Dryden operated two T-38s for a number of years, replacing them with newer F-18s. However, the cost of maintaining and operating the F-18s make the fuel-friendly, lower maintenance T-38 an attractive addition to Dryden's fleet. NASA has also operated a small fleet of T-38s for pilot proficiency and training for astronauts at the Johnson Space Center in Texas since the mid-1960s. |
Photo Date |
February 24, 2005 |
|
X-48C in Langley Full-Scale
An historic wind tunnel at N
9/4/09
Description |
An historic wind tunnel at NASA's Langley Research Center in Hampton, Va., is helping test the prototype of a new, more fuel-efficient, quieter aircraft design. Boeing Research & Technology, Huntington Beach, Calif., has partnered with NASA's Aeronautics Research Mission Directorate and the U.S. Air Force Research Laboratory, Wright Patterson Air Force Base, Ohio, to explore and validate the structural, aerodynamic and operational advantages of an advanced hybrid wing body concept called the blended wing body or BWB. NASA is flight testing one version of a 21-foot (6.4 m) wingspan BWB prototype, called the X-48B, at NASA's Dryden Flight Research Center, at Edwards AFB, Calif. The other one being tested in the Langley Full-Scale Tunnel is the X-48C. It has been modified to make it quieter. Those modifications include reducing the number of engines from three to two and the installation of noise-shielding vertical fins. The wind tunnel tests are assessing the aerodynamic effects of those modifications. NASA Langley owns the tunnel, but leased it to Old Dominion University in Norfolk, Va., for more than 10 years for research and student engineering training. Cranfield Aerospace Ltd., Cranfield, England, built the ground-breaking prototypes to Boeing Research & Technology's specifications. Made primarily of advanced lightweight composite materials, the prototypes weigh about 400 pounds (181 kg) each. The Air Force is interested in a full-scale version's potential as a multi-role, long-range, high-capacity military aircraft. This is the second time this aircraft has been put through its paces at the historic tunnel that was built in 1930 and has been used to test everything from World War II fighters, to the Mercury capsule, to concepts for a supersonic transport. In 2006, preliminary tests helped engineers determine how it would fly during remotely piloted flights. Blended wing body designs are different than traditional tube and wing aircraft. One is that they rely primarily on multiple control surfaces on the wing for stability and control. Another is that they blend tube and wings for lower drag and better lift. Credit: NASA/Sean Smith |
Date |
9/4/09 |
|
Photo Description |
NASA Dryden's T-38 Talon trainer jet in flight over the main base complex at Edwards Air Force Base. Formerly at NASA's Langley Research Center, this Northrop T-38 Talon is now used for mission support and pilot proficiency at the Dryden Flight Research Center. |
Project Description |
Formerly assigned to NASA's Langley Research Center in Hampton, Va., the T-38 aircraft had supported various aeronautics research projects there for a number of years. The aircraft is used by NASA Dryden's research pilots for proficiency and mission support flights. Dryden operated two T-38s for a number of years, replacing them with newer F-18s. However, the cost of maintaining and operating the F-18s make the fuel-friendly, lower maintenance T-38 an attractive addition to Dryden's fleet. NASA has also operated a small fleet of T-38s for pilot proficiency and training for astronauts at the Johnson Space Center in Texas since the mid-1960s. |
Photo Date |
May 5, 2006 |
|
Photo Description |
NASA Dryden's T-38 Talon trainer aircraft in flight near Edwards Air Force Base. Formerly at NASA's Langley Research Center, this Northrop T-38 Talon is now used for mission support and pilot proficiency at the Dryden Flight Research Center. |
Project Description |
Formerly assigned to NASA's Langley Research Center in Hampton, Va., the T-38 aircraft had supported various aeronautics research projects there for a number of years. The aircraft is used by NASA Dryden's research pilots for proficiency and mission support flights. Dryden operated two T-38s for a number of years, replacing them with newer F-18s. However, the cost of maintaining and operating the F-18s make the fuel-friendly, lower maintenance T-38 an attractive addition to Dryden's fleet. NASA has also operated a small fleet of T-38s for pilot proficiency and training for astronauts at the Johnson Space Center in Texas since the mid-1960s. |
Photo Date |
May 5, 2006 |
|
Photo Description |
NASA Dryden's T-38 trainer aircraft in flight over Cuddeback Dry Lake in Southern California. Formerly at NASA's Langley Research Center, this Northrop T-38 Talon is now used for mission support and pilot proficiency at the Dryden Flight Research Center. |
Project Description |
Formerly assigned to NASA's Langley Research Center in Hampton, Va., the T-38 aircraft had supported various aeronautics research projects there for a number of years. The aircraft is used by NASA Dryden's research pilots for proficiency and mission support flights. Dryden operated two T-38s for a number of years, replacing them with newer F-18s. However, the cost of maintaining and operating the F-18s make the fuel-friendly, lower maintenance T-38 an attractive addition to Dryden's fleet. NASA has also operated a small fleet of T-38s for pilot proficiency and training for astronauts at the Johnson Space Center in Texas since the mid-1960s. |
Photo Date |
May 5, 2006 |
|
Operation Ice Bridge 2009
ED09-0284-3 Glen Sachse of N
10/8/09
Description |
ED09-0284-3 Glen Sachse of NASA's Langley Research Center adjusts the Differential Absorption CO Measurement, or DACOM, instrument mounted in NASA's DC-8 flying laboratory in preparation for the Operation Ice Bridge deployment to the Antarctic. DACOM measures carbon monoxide, nitrous oxide and methane during the Operation Ice Bridge mission to the Antarctic. September 29, 2009 NASA photo / Tom Tschida |
Date |
10/8/09 |
|
NASA Dryden Flight Research
Photo Description |
NASA Dryden Flight Research Center's chief pilot Gordon Fullerton in the cockpit of the center's T-38 Talon mission support aircraft. |
Project Description |
A sleek, supersonic T-38 trainer jet is taxied into the parking ramp at NASA's Dryden Flight Research Center by Dryden's chief pilot Gordon Fullerton, marking the return of the type to Dryden for the first time in more than 10 years. Formerly assigned to NASA's Langley Research Center in Hampton, Va., the aircraft had supported various aeronautics research projects there for a number of years. The aircraft will be used by NASA Dryden's research pilots for proficiency and mission support flights. Dryden operated two T-38s for a number of years, replacing them with newer F-18s. However, the cost of maintaining and operating the F-18s make the fuel-friendly, lower maintenance T-38 an attractive addition to Dryden's fleet. NASA has also operated a small fleet of T-38s for pilot proficiency and training for astronauts at the Johnson Space Center in Texas since the mid-1960s. |
Photo Date |
February 24, 2005 |
|
History This Week: Sept. 30,
Five NACA engineers, headed
9/30/08
Description |
Five NACA engineers, headed by Walt Williams, arrived at Muroc Army Airfield (now Edwards AFB) about this date from Langley Memorial Aeronautical Laboratory, VA, to prepare for X-1 supersonic research flights in joint NACA-Army Air Forces program. This the first NACA-NASA presence is established at the Mojave Desert site. (Note: Some sources report the arrival of thirteen individuals on Sept. 30, but an early chronology shows only the original five, with a total of 13 NACA people not present at Muroc until December.) NASA Photo E70-21427 |
Date |
9/30/08 |
|
Photo Description |
Pilot Gordon Fullerton taxies NASA Dryden's "newest" mission support aircraft, a T-38 Talon, into position on the ramp upon its arrival on February 24, 2005. |
Project Description |
A sleek, supersonic T-38 trainer jet is taxied into the parking ramp at NASA's Dryden Flight Research Center by Dryden's chief pilot Gordon Fullerton, marking the return of the type to Dryden for the first time in more than 10 years. Formerly assigned to NASA's Langley Research Center in Hampton, Va., the aircraft had supported various aeronautics research projects there for a number of years. The aircraft will be used by NASA Dryden's research pilots for proficiency and mission support flights. Dryden operated two T-38s for a number of years, replacing them with newer F-18s. However, the cost of maintaining and operating the F-18s make the fuel-friendly, lower maintenance T-38 an attractive addition to Dryden's fleet. NASA has also operated a small fleet of T-38s for pilot proficiency and training for astronauts at the Johnson Space Center in Texas since the mid-1960s. |
Photo Date |
February 24, 2005 |
|
Dryden's David Bushman expla
Photo Description |
Puffy white clouds and a flooded lakebed form a backdrop as a T-38 support aircraft taxies across the ramp in front of NASA's Boeing 747 Shuttle Carrier Aircraft. |
Project Description |
A sleek, supersonic T-38 trainer jet is taxied into the parking ramp at NASA's Dryden Flight Research Center by Dryden's chief pilot Gordon Fullerton, marking the return of the type to Dryden for the first time in more than 10 years. Formerly assigned to NASA's Langley Research Center in Hampton, Va., the aircraft had supported various aeronautics research projects there for a number of years. The aircraft will be used by NASA Dryden's research pilots for proficiency and mission support flights. Dryden operated two T-38s for a number of years, replacing them with newer F-18s. However, the cost of maintaining and operating the F-18s make the fuel-friendly, lower maintenance T-38 an attractive addition to Dryden's fleet. NASA has also operated a small fleet of T-38s for pilot proficiency and training for astronauts at the Johnson Space Center in Texas since the mid-1960s. |
Photo Date |
February 24, 2005 |
|
F-18 HARV forebody surface f
Photo Date |
September 28, 1988 |
|
F-18 HARV smoke and tuft vor
Photo Date |
April 14, 1989 |
|
F-18 HARV smoke and tuft flo
Photo Date |
April 14, 1989 |
|
Dryden and Victory welcomed
Title |
Dryden and Victory welcomed by Reid |
Full Description |
Hugh L. Dryden (left), George Lewis's successor as the NACA's director of research, arrives with John F. Victory, the NACA's executive secretary, for a tour of the Langley Memorial Aeronautical Laboratory (LMAL). Welcoming Dryden and Victory is engineer-in-charge Henry Reid. |
Date |
09/08/1947 |
NASA Center |
Langley Research Center |
|
ER-2
News Release 06-25P ER-2 Alo
7/1/08
Description |
News Release 06-25P ER-2 Aloft Again After a lengthy downtime for a major overhaul, NASA 806, one of NASA's two high-flying ER-2 Earth resources aircraft, took to the skies recently from NASA's Dryden Flight Research Center on its first science mission in over two years. The flight checked out the functionality of sensitive instruments that will calibrate and validate data from sensors installed on the recently launched CALIPSO and CloudSat weather, climate and air quality monitoring satellites during a series of missions led by NASA's Langley Research Center with support from the Jet Propulsion Laboratory in late July and August. CALIPSO, an acronym for Cloud-Aerosol Lidar and Infrared Pathfinder Satellite Observations, combines an active lidar instrument with passive infrared and visible-light imagers to probe the vertical structure and properties of thin clouds and aerosols (airborne particles). The complimentary CloudSat satellite carries a cloud profiling radar system that uses microwave energy to observe cloud particles and determine the mass of water and ice within clouds. The mission will provide the first global survey of cloud properties that are critical for understanding their effects on both weather and climate. Flying in formation with three other satellites, CALIPSO and CloudSat are expected to provide scientists and meteorologists with a greater understanding of our climate system. Photo Description NASA Dryden life support technician Jim Sokolik assists pressure-suited pilot Dee Porter into the cockpit of NASA's ER-2 Earth resources aircraft. July 13, 2006 NASA Photo / Jim Ross ED06-0117-13 |
Date |
7/1/08 |
|
Supercritical Wing - Winglet
In the late 1970s Richard Wh
1/5/09
Description |
In the late 1970s Richard Whitcomb of Langley Research Center, Hampton Va., developed winglets, which reduced drag on aircraft wings. They were the third of his major aeronautical discoveries. In the 1960s, he had originated the supercritical wing, an airfoil shape that reduced drag at speeds just below Mach 1. In the 1950s, Whitcomb developed the area rule concept, discovering that a narrowing in the fuselage over the wing reduced high-speed drag at transonic speeds. Winglets typically have supercritical airfoils and serve as end plates on the wing that stop the spanwise airflow down the wing while diminishing wingtip vortices. They also "fool" the wing into behaving as if it had a longer span, making the wing more efficient without the performance penalties of a longer wing. Whitcomb selected the best winglet shape for flight tests on a KC-135 tanker. These were large vertical fins installed on the tanker's wing tips. The modified KC-135 was flight-tested at Dryden during 1979 and 1980 and the data showed that the winglets provided a 7 percent improvement in range over that of the standard KC-135. The economic advantage eventually led to adoption of winglets on light aircraft, business jets, airliners and heavy military transports. Winglets were also retrofitted on older aircraft. While the KC-135 winglets were large, subsequent designs were smaller and lighter. Whitcomb led a team of researchers to develop and test a series of unique geometric airfoil shapes, or wing designs, that could be applied to subsonic transport to reduce drag at high speeds. The result was the supercritical airfoil. Compared with a conventional wing, the supercritical wing is flatter on the top and rounder on the bottom with a downward curve at the trailing edge. Dryden research flights validated that aircraft using the supercritical wing see increased cruising speed, improved fuel efficiency (about 15 percent), and better flight range than those using conventional wings. As a result, supercritical wings are now common on most modern subsonic military and commercial transports. Photo Description F-8 Supercritical Wing aircraft flights demonstrated increased cruising speed, improved fuel efficiency of about 7 percent, and better flight range than those made with conventional wings. As a result, supercritical wings are now common on most modern subsonic commercial transports. NASA Photo |
Date |
1/5/09 |
|
Hyper-X and Pegasus Launch V
Photo Description |
The configuration of the X-43A Hypersonic Experimental Research Vehicle, or Hyper-X, attached to a Pegasus launch vehicle is displayed in this three-foot-long model at NASA's Dryden Flight Research Center, Edwards, California. |
Project Description |
Hyper-X, the flight vehicle for which is designated as X-43A, is an experimental flight-research program seeking to demonstrate airframe-integrated, "air-breathing" engine technologies that promise to increase payload capacity for future vehicles, including hypersonic aircraft (faster than Mach 5) and reusable space launchers. This multiyear program is currently underway at NASA Dryden Flight Research Center, Edwards, California. The Hyper-X schedule calls for its first flight later this year (2000). Hyper-X is a joint program, with Dryden sharing responsibility with NASA's Langley Research Center, Hampton, Virginia. Dryden's primary role is to fly three unpiloted X-43A research vehicles to validate engine technologies and hypersonic design tools as well as the hypersonic test facility at Langley. Langley manages the program and leads the technology development effort. The Hyper-X Program seeks to significantly expand the speed boundaries of air-breathing propulsion by being the first aircraft to demonstrate an airframe-integrated, scramjet-powered free flight. Scramjets (supersonic-combustion ramjets) are ramjet engines in which the airflow through the whole engine remains supersonic. Scramjet technology is challenging because only limited testing can be performed in ground facilities. Long duration, full-scale testing requires flight research. Scramjet engines are air-breathing, capturing their oxygen from the atmosphere. Current spacecraft, such as the Space Shuttle, are rocket powered, so they must carry both fuel and oxygen for propulsion. Scramjet technology-based vehicles need to carry only fuel. By eliminating the need to carry oxygen, future hypersonic vehicles will be able to carry heavier payloads. Another unique aspect of the X-43A vehicle is the airframe integration. The body of the vehicle itself forms critical elements of the engine. The forebody acts as part of the intake for airflow and the aft section serves as the nozzle. The X-43A vehicles were manufactured by Micro Craft, Inc., Tullahoma, Tennessee. Orbital Sciences Corporation, Chandler, Arizona, built the Pegasus rocket booster used to launch the X-43 vehicles. For the Dryden research flights, the Pegasus rocket booster and attached X-43 will be air launched by Dryden's B-52 "Mothership." After release from the B-52, the booster will accelerate the X-43A vehicle to the established test conditions (Mach 7 to 10) at an altitude of approximately 100,000 feet where the X-43 will separate from the booster and fly under its own power and preprogrammed control. |
Photo Date |
May 1997 |
|
Hyper-X and Pegasus Launch V
Photo Description |
The configuration of the X-43A Hypersonic Experimental Research Vehicle, or Hyper-X, attached to a Pegasus launch vehicle is displayed in this three-foot-long model at NASA's Dryden Flight Research Center, Edwards, California. |
Project Description |
Hyper-X, the flight vehicle for which is designated as X-43A, is an experimental flight-research program seeking to demonstrate airframe-integrated, "air-breathing" engine technologies that promise to increase payload capacity for future vehicles, including hypersonic aircraft (faster than Mach 5) and reusable space launchers. This multiyear program is currently underway at NASA Dryden Flight Research Center, Edwards, California. The Hyper-X schedule calls for its first flight later this year (2000). Hyper-X is a joint program, with Dryden sharing responsibility with NASA's Langley Research Center, Hampton, Virginia. Dryden's primary role is to fly three unpiloted X-43A research vehicles to validate engine technologies and hypersonic design tools as well as the hypersonic test facility at Langley. Langley manages the program and leads the technology development effort. The Hyper-X Program seeks to significantly expand the speed boundaries of air-breathing propulsion by being the first aircraft to demonstrate an airframe-integrated, scramjet-powered free flight. Scramjets (supersonic-combustion ramjets) are ramjet engines in which the airflow through the whole engine remains supersonic. Scramjet technology is challenging because only limited testing can be performed in ground facilities. Long duration, full-scale testing requires flight research. Scramjet engines are air-breathing, capturing their oxygen from the atmosphere. Current spacecraft, such as the Space Shuttle, are rocket powered, so they must carry both fuel and oxygen for propulsion. Scramjet technology-based vehicles need to carry only fuel. By eliminating the need to carry oxygen, future hypersonic vehicles will be able to carry heavier payloads. Another unique aspect of the X-43A vehicle is the airframe integration. The body of the vehicle itself forms critical elements of the engine. The forebody acts as part of the intake for airflow and the aft section serves as the nozzle. The X-43A vehicles were manufactured by Micro Craft, Inc., Tullahoma, Tennessee. Orbital Sciences Corporation, Chandler, Arizona, built the Pegasus rocket booster used to launch the X-43 vehicles. For the Dryden research flights, the Pegasus rocket booster and attached X-43 will be air launched by Dryden's B-52 "Mothership." After release from the B-52, the booster will accelerate the X-43A vehicle to the established test conditions (Mach 7 to 10) at an altitude of approximately 100,000 feet where the X-43 will separate from the booster and fly under its own power and preprogrammed control. |
Photo Date |
May 1997 |
|
Hyper-X and Pegasus Launch V
Photo Description |
The configuration of the X-43A Hypersonic Experimental Research Vehicle, or Hyper-X, attached to a Pegasus launch vehicle is displayed in this three-foot-long model at NASA's Dryden Flight Research Center, Edwards, California. |
Project Description |
Hyper-X, the flight vehicle for which is designated as X-43A, is an experimental flight-research program seeking to demonstrate airframe-integrated, "air-breathing" engine technologies that promise to increase payload capacity for future vehicles, including hypersonic aircraft (faster than Mach 5) and reusable space launchers. This multiyear program is currently underway at NASA Dryden Flight Research Center, Edwards, California. The Hyper-X schedule calls for its first flight later this year (2000). Hyper-X is a joint program, with Dryden sharing responsibility with NASA's Langley Research Center, Hampton, Virginia. Dryden's primary role is to fly three unpiloted X-43A research vehicles to validate engine technologies and hypersonic design tools as well as the hypersonic test facility at Langley. Langley manages the program and leads the technology development effort. The Hyper-X Program seeks to significantly expand the speed boundaries of air-breathing propulsion by being the first aircraft to demonstrate an airframe-integrated, scramjet-powered free flight. Scramjets (supersonic-combustion ramjets) are ramjet engines in which the airflow through the whole engine remains supersonic. Scramjet technology is challenging because only limited testing can be performed in ground facilities. Long duration, full-scale testing requires flight research. Scramjet engines are air-breathing, capturing their oxygen from the atmosphere. Current spacecraft, such as the Space Shuttle, are rocket powered, so they must carry both fuel and oxygen for propulsion. Scramjet technology-based vehicles need to carry only fuel. By eliminating the need to carry oxygen, future hypersonic vehicles will be able to carry heavier payloads. Another unique aspect of the X-43A vehicle is the airframe integration. The body of the vehicle itself forms critical elements of the engine. The forebody acts as part of the intake for airflow and the aft section serves as the nozzle. The X-43A vehicles were manufactured by Micro Craft, Inc., Tullahoma, Tennessee. Orbital Sciences Corporation, Chandler, Arizona, built the Pegasus rocket booster used to launch the X-43 vehicles. For the Dryden research flights, the Pegasus rocket booster and attached X-43 will be air launched by Dryden's B-52 "Mothership." After release from the B-52, the booster will accelerate the X-43A vehicle to the established test conditions (Mach 7 to 10) at an altitude of approximately 100,000 feet where the X-43 will separate from the booster and fly under its own power and preprogrammed control. |
Photo Date |
May 1997 |
|
JetStar
Photo Description |
The Dryden C-140 JetStar during testing of advanced propfan designs. Dryden conducted flight research in 1981-1982 on several designs. The technology was developed under the direction of the Lewis Research Center (today the Glenn Research Center, Cleveland, OH) under the Advanced Turboprop Program. Under that program, Langley Research Center in Virginia oversaw work on accoustics and noise reduction. These efforts were intended to develop a high-speed and fuel-efficient turboprop system. |
Project Description |
NASA's Dryden Flight Research Facility (later the Dryden Flight Research Center, Edwards, CA), in co-operation with the Lewis Research Center, investigated the acoustic characteristics of a series of subscale advanced design propellors in the early eighties. These propellors were designed to rotate at a tip speed faster than the speed of sound. They are, in effect, a "swept back wing" version of a propellor. The tests were conducted on Dryden's C-140 Jetstar, seen here on a research flight over the Mojave desert. The JetStar was modified with the installation of an air turbine drive system. The drive motor, with a 24 inch test propellor, was mounted in a pylon atop the JetStar. The JetStar was equipped with an array of 28 microphones flush-mounted in the fuselage of the aircraft beneath the propellor. Microphones mounted on the wings and on accompanying chase aircraft provided far-field acoustic data. In the 1960s, the same JetStar was equipped with an electronic variable stability flight control system. Called th (GPAS), the aircraft could duplicate the flight characteristics of a wide variety of advanced aircraft and was used for supersonic transport and general aviation research and as a training and support system for Space Shuttle Approach and Landing Tests at Dryden in 1977. In 1985, the JetStar's wings were modified with suction and spray devices in a laminar (smooth) air flow program to study ways of improving the flow of air over the wings of airliners. The program also studied ways of reducing the collection of ice and insects on airliner wings. |
Photo Date |
May 21, 1981 |
|
Segment for NASA 360, INDY C
2008 Videographer of the Yea
Description |
2008 Videographer of the Year, 3rd place, production category. By Michael Bibbo, LaRC. |
|
Lockheed Electra - aerial vi
Lockheed Electra - takeoff f
Technicians inspect the sub-
Photo Description |
Technicians inspect the sub-scale X-48B Blended Wing Body concept demonstrator in the full-scale wind tunnel at NASA's Langley Research Center. Researchers at NASA's Langley Research Center in Hampton, Va., are testing the a 21-foot wingspan 8.5 percent scale prototype of a blended wing body aircraft in Langley's historic full-scale wind tunnel. Boeing Phantom Works has partnered with NASA and the Air Force Research Laboratory to study the structural, aerodynamic and operational advantages of the advanced aircraft concept, a cross between a conventional plane and a flying wing design. The Air Force has designated the prototype the X-48B based on its interest in the design's potential as a multi-role, long-range, high-capacity military transport aircraft. A second X-48B blended-wing body prototype is due to arrive at NASA Dryden Flight Research Center in May, and after installation of test instrumentation and extensive checkout, begin flight tests later this year. (Boeing photo # K636682-01B) |
Project Description |
unknown |
Photo Date |
May, 2006 |
|
F-18 HARV instrumentation mo
Photo Date |
October 15, 1993 |
|
F-18 HARV in flight with act
F-18 HARV on ramp close-up o
Photo Date |
March 24, 1995 |
|
Project Description |
The F-101A was a single-seat fighter powered by two Pratt and Whitney engines. A triangular-shaped inlet with elliptical lips was located in each wing root, and supplied air to each engine. The NACA High-Speed Flight Station conducted research on inlet-flow distortion and total pressure recovery at the engine compressor face on the F-101A and two other fighter type aircraft. The McDonnell F-101A Voodoo was at NACA High-Speed Flight Station for a period of time until being transferred to NACA Langley Aeronautical Laboratory in 1956. |
Photo Date |
August 10, 1956 |
|
Project Description |
The F-101A was a single-seat fighter powered by two Pratt and Whitney engines. A triangular-shaped inlet with elliptical lips was located in each wing root, and supplied air to each engine. The NACA High-Speed Flight Station conducted research on inlet-flow distortion and total pressure recovery at the engine compressor face on the F-101A and two other fighter type aircraft. The McDonnell F-101A Voodoo was at NACA High-Speed Flight Station for a period of time until being transferred to NACA Langley Aeronautical Laboratory in 1956. |
Photo Date |
August 10, 1956 |
|
Ares I-X Coming Together
The Ares I-X launch abort sy
01/30/09
Description |
The Ares I-X launch abort system (LAS) simulator joins rocket elements from NASA Glenn in the cavernous Vehicle Assembly Building at the Kennedy Space Center. The 53-foot (16.15-meter) LAS, along with the crew module (CM) simulator will make up the nose of Ares I-X. The LAS and CM simulators were designed and built at NASA Langley Research Center. Credit: NASA/Sean Smith |
Date |
01/30/09 |
|
Ares I-X Coming Together
The Ares I-X launch abort sy
01/30/09
Description |
The Ares I-X launch abort system (LAS) simulator joins rocket elements from NASA Glenn in the cavernous Vehicle Assembly Building at the Kennedy Space Center. The 53-foot (16.15-meter) LAS, along with the crew module (CM) simulator will make up the nose of Ares I-X. The LAS and CM simulators were designed and built at NASA Langley Research Center. Credit: NASA/Sean Smith |
Date |
01/30/09 |
|
Ares I-X Coming Together
The Ares I-X launch abort sy
01/30/09
Description |
The Ares I-X launch abort system (LAS) simulator joins rocket elements from NASA Glenn in the cavernous Vehicle Assembly Building at the Kennedy Space Center. The 53-foot (16.15-meter) LAS, along with the crew module (CM) simulator will make up the nose of Ares I-X. The LAS and CM simulators were designed and built at NASA Langley Research Center. Credit: NASA/Sean Smith |
Date |
01/30/09 |
|
Ares I-X Coming Together
The Ares I-X launch abort sy
01/30/09
Description |
The Ares I-X launch abort system (LAS) simulator joins rocket elements from NASA Glenn in the cavernous Vehicle Assembly Building at the Kennedy Space Center. The 53-foot (16.15-meter) LAS, along with the crew module (CM) simulator will make up the nose of Ares I-X. The LAS and CM simulators were designed and built at NASA Langley Research Center. Credit: NASA/Sean Smith |
Date |
01/30/09 |
|
Ares I-X Coming Together
The Ares I-X launch abort sy
01/30/09
Description |
The Ares I-X launch abort system (LAS) simulator joins rocket elements from NASA Glenn in the cavernous Vehicle Assembly Building at the Kennedy Space Center. The 53-foot (16.15-meter) LAS, along with the crew module (CM) simulator will make up the nose of Ares I-X. The LAS and CM simulators were designed and built at NASA Langley Research Center. Credit: NASA/Sean Smith |
Date |
01/30/09 |
|
Ares I-X Coming Together
The Ares I-X launch abort sy
01/30/09
Description |
The Ares I-X launch abort system (LAS) simulator joins rocket elements from NASA Glenn in the cavernous Vehicle Assembly Building at the Kennedy Space Center. The 53-foot (16.15-meter) LAS, along with the crew module (CM) simulator will make up the nose of Ares I-X. The LAS and CM simulators were designed and built at NASA Langley Research Center. Credit: NASA/Sean Smith |
Date |
01/30/09 |
|
Ares I-X Coming Together
The Ares I-X launch abort sy
01/30/09
Description |
The Ares I-X launch abort system (LAS) simulator joins rocket elements from NASA Glenn in the cavernous Vehicle Assembly Building at the Kennedy Space Center. The 53-foot (16.15-meter) LAS, along with the crew module (CM) simulator will make up the nose of Ares I-X. The LAS and CM simulators were designed and built at NASA Langley Research Center. Credit: NASA/Sean Smith |
Date |
01/30/09 |
|
Photo Description |
NASA's Dryden Flight Research Center marked its 60th anniversary as the aerospace agency's lead center for atmospheric flight research and operations in 2006. In connection with that milestone, hundreds of the center's staff and retirees gathered in nearby Lancaster, Calif., in November 2006 to reflect on the center's challenges and celebrate its accomplishments over its six decades of advancing the state-of-the-art in aerospace technology. The center had its beginning in 1946 when a few engineers from the National Advisory Committee for Aeronautics' Langley Memorial Aeronautical Laboratory were detailed to Muroc Army Air Base (now Edwards Air Force Base) in Southern California's high desert to support the joint Army Air Force / NACA / Bell Aircraft XS-1 research airplane program. Since that inauspicious beginning, the center has been at the forefront of many of the advances in aerospace technology by validating advanced concepts through actual in-flight research and testing. Dryden is uniquely situated to take advantage of the excellent year-round flying weather, remote area, and visibility to test some of the nation?s most exciting aerospace vehicles. Today, NASA Dryden is NASA's premier flight research and test organization, continuing to push the envelope in the validation of high-risk aerospace technology and space exploration concepts, and in conducting airborne environmental and space science missions in the 21st century. |
Project Description |
unknown |
Photo Date |
November 4, 2006 |
|
X-43A/Hyper-X Vehicle Arrive
Photo Description |
A close-up of the X-43A Hypersonic Experimental Vehicle, or "Hyper-X," in its protective shipping framework as it arrives at the Dryden Flight Research Center in October 1999. The X-43A was developed to research a dual-mode ramjet/scramjet propulsion system at speeds from Mach 7 up to Mach 10 (7 to 10 times the speed of sound, which varies with temperature and altitude). |
Project Description |
Hyper-X, the flight vehicle for which is designated as X-43A, is an experimental flight-research program seeking to demonstrate airframe-integrated, "air-breathing" engine technologies that promise to increase payload capacity for future vehicles, including hypersonic aircraft (faster than Mach 5) and reusable space launchers. This multiyear program is currently underway at NASA Dryden Flight Research Center, Edwards, California. The Hyper-X schedule calls for its first flight later this year (2000). Hyper-X is a joint program, with Dryden sharing responsibility with NASA's Langley Research Center, Hampton, Virginia. Dryden's primary role is to fly three unpiloted X-43A research vehicles to validate engine technologies and hypersonic design tools as well as the hypersonic test facility at Langley. Langley manages the program and leads the technology development effort. The Hyper-X Program seeks to significantly expand the speed boundaries of air-breathing propulsion by being the first aircraft to demonstrate an airframe-integrated, scramjet-powered free flight. Scramjets (supersonic-combustion ramjets) are ramjet engines in which the airflow through the whole engine remains supersonic. Scramjet technology is challenging because only limited testing can be performed in ground facilities. Long duration, full-scale testing requires flight research. Scramjet engines are air-breathing, capturing their oxygen from the atmosphere. Current spacecraft, such as the Space Shuttle, are rocket powered, so they must carry both fuel and oxygen for propulsion. Scramjet technology-based vehicles need to carry only fuel. By eliminating the need to carry oxygen, future hypersonic vehicles will be able to carry heavier payloads. Another unique aspect of the X-43A vehicle is the airframe integration. The body of the vehicle itself forms critical elements of the engine. The forebody acts as part of the intake for airflow and the aft section serves as the nozzle. The X-43A vehicles were manufactured by Micro Craft, Inc., Tullahoma, Tennessee. Orbital Sciences Corporation, Chandler, Arizona, built the Pegasus rocket booster used to launch the X-43 vehicles. For the Dryden research flights, the Pegasus rocket booster and attached X-43 will be air launched by Dryden's B-52 "Mothership." After release from the B-52, the booster will accelerate the X-43A vehicle to the established test conditions (Mach 7 to 10) at an altitude of approximately 100,000 feet where the X-43 will separate from the booster and fly under its own power and preprogrammed control. |
Photo Date |
October 1999 |
|
X-43A/Hyper-X Vehicle Arrive
Photo Description |
A head-on view of the X-43A Hypersonic Experimental Vehicle, or "Hyper-X," in its protective shipping framework as it arrives at the Dryden Flight Research Center in October 1999. The X-43A was developed to research a dual-mode ramjet/scramjet propulsion system at speeds from Mach 7 up to Mach 10 (7 to 10 times the speed of sound, which varies with temperature and altitude). |
Project Description |
Hyper-X, the flight vehicle for which is designated as X-43A, is an experimental flight-research program seeking to demonstrate airframe-integrated, "air-breathing" engine technologies that promise to increase payload capacity for future vehicles, including hypersonic aircraft (faster than Mach 5) and reusable space launchers. This multiyear program is currently underway at NASA Dryden Flight Research Center, Edwards, California. The Hyper-X schedule calls for its first flight later this year (2000). Hyper-X is a joint program, with Dryden sharing responsibility with NASA's Langley Research Center, Hampton, Virginia. Dryden's primary role is to fly three unpiloted X-43A research vehicles to validate engine technologies and hypersonic design tools as well as the hypersonic test facility at Langley. Langley manages the program and leads the technology development effort. The Hyper-X Program seeks to significantly expand the speed boundaries of air-breathing propulsion by being the first aircraft to demonstrate an airframe-integrated, scramjet-powered free flight. Scramjets (supersonic-combustion ramjets) are ramjet engines in which the airflow through the whole engine remains supersonic. Scramjet technology is challenging because only limited testing can be performed in ground facilities. Long duration, full-scale testing requires flight research. Scramjet engines are air-breathing, capturing their oxygen from the atmosphere. Current spacecraft, such as the Space Shuttle, are rocket powered, so they must carry both fuel and oxygen for propulsion. Scramjet technology-based vehicles need to carry only fuel. By eliminating the need to carry oxygen, future hypersonic vehicles will be able to carry heavier payloads. Another unique aspect of the X-43A vehicle is the airframe integration. The body of the vehicle itself forms critical elements of the engine. The forebody acts as part of the intake for airflow and the aft section serves as the nozzle. The X-43A vehicles were manufactured by Micro Craft, Inc., Tullahoma, Tennessee. Orbital Sciences Corporation, Chandler, Arizona, built the Pegasus rocket booster used to launch the X-43 vehicles. For the Dryden research flights, the Pegasus rocket booster and attached X-43 will be air launched by Dryden's B-52 "Mothership." After release from the B-52, the booster will accelerate the X-43A vehicle to the established test conditions (Mach 7 to 10) at an altitude of approximately 100,000 feet where the X-43 will separate from the booster and fly under its own power and preprogrammed control. |
Photo Date |
October 1999 |
|
X-43A/Hyper-X Vehicle Arrive
Photo Description |
The X-43A Hypersonic Experimental Vehicle, or "Hyper-X," carefully packed in a protective shipping framework, is unloaded from a container after its arrival at NASA's Dryden Flight Research Center in October 1999. The X-43A was developed to research a dual-mode ramjet/scramjet propulsion system at speeds from Mach 7 up to Mach 10 (7 to 10 times the speed of sound, which varies with temperature and altitude). |
Project Description |
Hyper-X, the flight vehicle for which is designated as X-43A, is an experimental flight-research program seeking to demonstrate airframe-integrated, "air-breathing" engine technologies that promise to increase payload capacity for future vehicles, including hypersonic aircraft (faster than Mach 5) and reusable space launchers. This multiyear program is currently underway at NASA Dryden Flight Research Center, Edwards, California. The Hyper-X schedule calls for its first flight later this year (2000). Hyper-X is a joint program, with Dryden sharing responsibility with NASA's Langley Research Center, Hampton, Virginia. Dryden's primary role is to fly three unpiloted X-43A research vehicles to validate engine technologies and hypersonic design tools as well as the hypersonic test facility at Langley. Langley manages the program and leads the technology development effort. The Hyper-X Program seeks to significantly expand the speed boundaries of air-breathing propulsion by being the first aircraft to demonstrate an airframe-integrated, scramjet-powered free flight. Scramjets (supersonic-combustion ramjets) are ramjet engines in which the airflow through the whole engine remains supersonic. Scramjet technology is challenging because only limited testing can be performed in ground facilities. Long duration, full-scale testing requires flight research. Scramjet engines are air-breathing, capturing their oxygen from the atmosphere. Current spacecraft, such as the Space Shuttle, are rocket powered, so they must carry both fuel and oxygen for propulsion. Scramjet technology-based vehicles need to carry only fuel. By eliminating the need to carry oxygen, future hypersonic vehicles will be able to carry heavier payloads. Another unique aspect of the X-43A vehicle is the airframe integration. The body of the vehicle itself forms critical elements of the engine. The forebody acts as part of the intake for airflow and the aft section serves as the nozzle. The X-43A vehicles were manufactured by Micro Craft, Inc., Tullahoma, Tennessee. Orbital Sciences Corporation, Chandler, Arizona, built the Pegasus rocket booster used to launch the X-43 vehicles. For the Dryden research flights, the Pegasus rocket booster and attached X-43 will be air launched by Dryden's B-52 "Mothership." After release from the B-52, the booster will accelerate the X-43A vehicle to the established test conditions (Mach 7 to 10) at an altitude of approximately 100,000 feet where the X-43 will separate from the booster and fly under its own power and preprogrammed control. |
Photo Date |
October 1999 |
|
Ares I-X Coming Together
Sunrise at NASA's Kennedy Sp
01/30/09
Description |
Sunrise at NASA's Kennedy Space Center the day the Ares I-X crew module and launch abort system simulators arrived from NASA Langley. Credit: NASA/Sean Smith |
Date |
01/30/09 |
|
F-18 HARV final flight over
F-18 HARV final flight over
Photo Description |
Attached to the same B-52B mothership that once launched X-15 research aircraft in the 1960s, NASA's third X-43A performed a captive carry evaluation flight from Edwards Air Force Base, California on September 27, 2004. The X-43 remained mated to the B-52 throughout this mission, intended to check its readiness for launch scheduled later in the fall. |
Project Description |
The X-43A is powered by a revolutionary supersonic-combustion ramjet - or "scramjet" - engine. If successful, the Mach 10 flight will break all speed records for an aircraft powered by an air-breathing engine. The X-43 is part of the Hyper-X hypersonic research program led by NASA's Aeronautics Research Mission Directorate, and operated jointly by NASA's Langley Research Center, Hampton, Va., and Dryden Flight Research Center, Edwards, Calif. The program aims to demonstrate air-breathing engine technologies that promise to increase payload capacity - or reduce vehicle size for the same payload - for future hypersonic aircraft and reusable space launch vehicles. |
Photo Date |
September 27, 2004 |
|
Photo Description |
Attached to the same B-52B mothership that once launched X-15 research aircraft in the 1960s, NASA's third X-43A performed a captive carry evaluation flight from Edwards Air Force Base, California on September 27, 2004. The X-43 remained mated to the B-52 throughout this mission, intended to check its readiness for launch scheduled later in the fall. |
Project Description |
The X-43A is powered by a revolutionary supersonic-combustion ramjet - or "scramjet" - engine. If successful, the Mach 10 flight will break all speed records for an aircraft powered by an air-breathing engine. The X-43 is part of the Hyper-X hypersonic research program led by NASA's Aeronautics Research Mission Directorate, and operated jointly by NASA's Langley Research Center, Hampton, Va., and Dryden Flight Research Center, Edwards, Calif. The program aims to demonstrate air-breathing engine technologies that promise to increase payload capacity - or reduce vehicle size for the same payload - for future hypersonic aircraft and reusable space launch vehicles. |
Photo Date |
September 27, 2004 |
|
Hyper-X and Pegasus Launch V
Photo Description |
The configuration of the X-43A Hypersonic Experimental Research Vehicle, or Hyper-X, attached to a Pegasus launch vehicle is displayed in this side view of a three-foot-long model of the vehicle/booster combination at NASA's Dryden Flight Research Center, Edwards, California. |
Project Description |
Hyper-X, the flight vehicle for which is designated as X-43A, is an experimental flight-research program seeking to demonstrate airframe-integrated, "air-breathing" engine technologies that promise to increase payload capacity for future vehicles, including hypersonic aircraft (faster than Mach 5) and reusable space launchers. This multiyear program is currently underway at NASA Dryden Flight Research Center, Edwards, California. The Hyper-X schedule calls for its first flight later this year (2000). Hyper-X is a joint program, with Dryden sharing responsibility with NASA's Langley Research Center, Hampton, Virginia. Dryden's primary role is to fly three unpiloted X-43A research vehicles to validate engine technologies and hypersonic design tools as well as the hypersonic test facility at Langley. Langley manages the program and leads the technology development effort. The Hyper-X Program seeks to significantly expand the speed boundaries of air-breathing propulsion by being the first aircraft to demonstrate an airframe-integrated, scramjet-powered free flight. Scramjets (supersonic-combustion ramjets) are ramjet engines in which the airflow through the whole engine remains supersonic. Scramjet technology is challenging because only limited testing can be performed in ground facilities. Long duration, full-scale testing requires flight research. Scramjet engines are air-breathing, capturing their oxygen from the atmosphere. Current spacecraft, such as the Space Shuttle, are rocket powered, so they must carry both fuel and oxygen for propulsion. Scramjet technology-based vehicles need to carry only fuel. By eliminating the need to carry oxygen, future hypersonic vehicles will be able to carry heavier payloads. Another unique aspect of the X-43A vehicle is the airframe integration. The body of the vehicle itself forms critical elements of the engine. The forebody acts as part of the intake for airflow and the aft section serves as the nozzle. The X-43A vehicles were manufactured by Micro Craft, Inc., Tullahoma, Tennessee. Orbital Sciences Corporation, Chandler, Arizona, built the Pegasus rocket booster used to launch the X-43 vehicles. For the Dryden research flights, the Pegasus rocket booster and attached X-43 will be air launched by Dryden's B-52 "Mothership." After release from the B-52, the booster will accelerate the X-43A vehicle to the established test conditions (Mach 7 to 10) at an altitude of approximately 100,000 feet where the X-43 will separate from the booster and fly under its own power and preprogrammed control. |
Photo Date |
May 1997 |
|
Hyper-X and Pegasus Launch V
Photo Description |
A close-up view of the X-43A Hypersonic Experimental Research Vehicle, or Hyper-X, portion of a three-foot-long model of the vehicle/booster combination at NASA's Dryden Flight Research Center, Edwards, California. |
Project Description |
Hyper-X, the flight vehicle for which is designated as X-43A, is an experimental flight-research program seeking to demonstrate airframe-integrated, "air-breathing" engine technologies that promise to increase payload capacity for future vehicles, including hypersonic aircraft (faster than Mach 5) and reusable space launchers. This multiyear program is currently underway at NASA Dryden Flight Research Center, Edwards, California. The Hyper-X schedule calls for its first flight later this year (2000). Hyper-X is a joint program, with Dryden sharing responsibility with NASA's Langley Research Center, Hampton, Virginia. Dryden's primary role is to fly three unpiloted X-43A research vehicles to validate engine technologies and hypersonic design tools as well as the hypersonic test facility at Langley. Langley manages the program and leads the technology development effort. The Hyper-X Program seeks to significantly expand the speed boundaries of air-breathing propulsion by being the first aircraft to demonstrate an airframe-integrated, scramjet-powered free flight. Scramjets (supersonic-combustion ramjets) are ramjet engines in which the airflow through the whole engine remains supersonic. Scramjet technology is challenging because only limited testing can be performed in ground facilities. Long duration, full-scale testing requires flight research. Scramjet engines are air-breathing, capturing their oxygen from the atmosphere. Current spacecraft, such as the Space Shuttle, are rocket powered, so they must carry both fuel and oxygen for propulsion. Scramjet technology-based vehicles need to carry only fuel. By eliminating the need to carry oxygen, future hypersonic vehicles will be able to carry heavier payloads. Another unique aspect of the X-43A vehicle is the airframe integration. The body of the vehicle itself forms critical elements of the engine. The forebody acts as part of the intake for airflow and the aft section serves as the nozzle. The X-43A vehicles were manufactured by Micro Craft, Inc., Tullahoma, Tennessee. Orbital Sciences Corporation, Chandler, Arizona, built the Pegasus rocket booster used to launch the X-43 vehicles. For the Dryden research flights, the Pegasus rocket booster and attached X-43 will be air launched by Dryden's B-52 "Mothership." After release from the B-52, the booster will accelerate the X-43A vehicle to the established test conditions (Mach 7 to 10) at an altitude of approximately 100,000 feet where the X-43 will separate from the booster and fly under its own power and preprogrammed control. |
Photo Date |
May 1997 |
|
Pegasus Rocket Booster Being
Photo Description |
A close-up view of the front end of a Pegasus rocket booster being prepared by technicians at the Dryden Flight Research Center for flight tests with the X-43A "Hypersonic Experimental Vehicle," or "Hyper-X." The X-43A, which will be attached to the Pegasus booster and drop launched from NASA's B-52 mothership, was developed to research dual-mode ramjet/scramjet propulsion system at speeds from Mach 7 up to Mach 10 (7 to 10 times the speed of sound, which varies with temperature and altitude). |
Project Description |
Hyper-X, the flight vehicle for which is designated as X-43A, is an experimental flight-research program seeking to demonstrate airframe-integrated, "air-breathing" engine technologies that promise to increase payload capacity for future vehicles, including hypersonic aircraft (faster than Mach 5) and reusable space launchers. This multiyear program is currently underway at NASA Dryden Flight Research Center, Edwards, California. The Hyper-X schedule calls for its first flight later this year (2000). Hyper-X is a joint program, with Dryden sharing responsibility with NASA's Langley Research Center, Hampton, Virginia. Dryden's primary role is to fly three unpiloted X-43A research vehicles to validate engine technologies and hypersonic design tools as well as the hypersonic test facility at Langley. Langley manages the program and leads the technology development effort. The Hyper-X Program seeks to significantly expand the speed boundaries of air-breathing propulsion by being the first aircraft to demonstrate an airframe-integrated, scramjet-powered free flight. Scramjets (supersonic-combustion ramjets) are ramjet engines in which the airflow through the whole engine remains supersonic. Scramjet technology is challenging because only limited testing can be performed in ground facilities. Long duration, full-scale testing requires flight research. Scramjet engines are air-breathing, capturing their oxygen from the atmosphere. Current spacecraft, such as the Space Shuttle, are rocket powered, so they must carry both fuel and oxygen for propulsion. Scramjet technology-based vehicles need to carry only fuel. By eliminating the need to carry oxygen, future hypersonic vehicles will be able to carry heavier payloads. Another unique aspect of the X-43A vehicle is the airframe integration. The body of the vehicle itself forms critical elements of the engine. The forebody acts as part of the intake for airflow and the aft section serves as the nozzle. The X-43A vehicles were manufactured by Micro Craft, Inc., Tullahoma, Tennessee. Orbital Sciences Corporation, Chandler, Arizona, built the Pegasus rocket booster used to launch the X-43 vehicles. For the Dryden research flights, the Pegasus rocket booster and attached X-43 will be air launched by Dryden's B-52 "Mothership." After release from the B-52, the booster will accelerate the X-43A vehicle to the established test conditions (Mach 7 to 10) at an altitude of approximately 100,000 feet where the X-43 will separate from the booster and fly under its own power and preprogrammed control. |
Photo Date |
August 25, 1999 |
|
X-43A Vehicle During Ground
Photo Description |
The X-43A Hypersonic Experimental Vehicle, or "Hyper-X" is seen here undergoing ground testing at NASA's Dryden Flight Research Center, Edwards, California. The X-43A was developed to research a dual-mode ramjet/scramjet propulsion system at speeds from Mach 7 up to Mach 10 (7 to 10 times the speed of sound, which varies with temperature and altitude). |
Project Description |
Hyper-X, the flight vehicle for which is designated as X-43A, is an experimental flight-research program seeking to demonstrate airframe-integrated, "air-breathing" engine technologies that promise to increase payload capacity for future vehicles, including hypersonic aircraft (faster than Mach 5) and reusable space launchers. This multiyear program is currently underway at NASA Dryden Flight Research Center, Edwards, California. The Hyper-X schedule calls for its first flight later this year (2000). Hyper-X is a joint program, with Dryden sharing responsibility with NASA's Langley Research Center, Hampton, Virginia. Dryden's primary role is to fly three unpiloted X-43A research vehicles to validate engine technologies and hypersonic design tools as well as the hypersonic test facility at Langley. Langley manages the program and leads the technology development effort. The Hyper-X Program seeks to significantly expand the speed boundaries of air-breathing propulsion by being the first aircraft to demonstrate an airframe-integrated, scramjet-powered free flight. Scramjets (supersonic-combustion ramjets) are ramjet engines in which the airflow through the whole engine remains supersonic. Scramjet technology is challenging because only limited testing can be performed in ground facilities. Long duration, full-scale testing requires flight research. Scramjet engines are air-breathing, capturing their oxygen from the atmosphere. Current spacecraft, such as the Space Shuttle, are rocket powered, so they must carry both fuel and oxygen for propulsion. Scramjet technology-based vehicles need to carry only fuel. By eliminating the need to carry oxygen, future hypersonic vehicles will be able to carry heavier payloads. Another unique aspect of the X-43A vehicle is the airframe integration. The body of the vehicle itself forms critical elements of the engine. The forebody acts as part of the intake for airflow and the aft section serves as the nozzle. The X-43A vehicles were manufactured by Micro Craft, Inc., Tullahoma, Tennessee. Orbital Sciences Corporation, Chandler, Arizona, built the Pegasus rocket booster used to launch the X-43 vehicles. For the Dryden research flights, the Pegasus rocket booster and attached X-43 will be air launched by Dryden's B-52 "Mothership." After release from the B-52, the booster will accelerate the X-43A vehicle to the established test conditions (Mach 7 to 10) at an altitude of approximately 100,000 feet where the X-43 will separate from the booster and fly under its own power and preprogrammed control. |
Photo Date |
December 1999 |
|
X-43A Vehicle During Ground
Photo Description |
This photo shows a close-up, rear view of the X-43A Hypersonic Experimental Vehicle, or "Hyper-X" undergoing ground testing at NASA's Dryden Flight Research Center, Edwards, California in December 1999. The X-43A was developed to research a dual-mode ramjet/scramjet propulsion system at speeds from Mach 7 up to Mach 10 (7 to 10 times the speed of sound, which varies with temperature and altitude). |
Project Description |
Hyper-X, the flight vehicle for which is designated as X-43A, is an experimental flight-research program seeking to demonstrate airframe-integrated, "air-breathing" engine technologies that promise to increase payload capacity for future vehicles, including hypersonic aircraft (faster than Mach 5) and reusable space launchers. This multiyear program is currently underway at NASA Dryden Flight Research Center, Edwards, California. The Hyper-X schedule calls for its first flight later this year (2000). Hyper-X is a joint program, with Dryden sharing responsibility with NASA's Langley Research Center, Hampton, Virginia. Dryden's primary role is to fly three unpiloted X-43A research vehicles to validate engine technologies and hypersonic design tools as well as the hypersonic test facility at Langley. Langley manages the program and leads the technology development effort. The Hyper-X Program seeks to significantly expand the speed boundaries of air-breathing propulsion by being the first aircraft to demonstrate an airframe-integrated, scramjet-powered free flight. Scramjets (supersonic-combustion ramjets) are ramjet engines in which the airflow through the whole engine remains supersonic. Scramjet technology is challenging because only limited testing can be performed in ground facilities. Long duration, full-scale testing requires flight research. Scramjet engines are air-breathing, capturing their oxygen from the atmosphere. Current spacecraft, such as the Space Shuttle, are rocket powered, so they must carry both fuel and oxygen for propulsion. Scramjet technology-based vehicles need to carry only fuel. By eliminating the need to carry oxygen, future hypersonic vehicles will be able to carry heavier payloads. Another unique aspect of the X-43A vehicle is the airframe integration. The body of the vehicle itself forms critical elements of the engine. The forebody acts as part of the intake for airflow and the aft section serves as the nozzle. The X-43A vehicles were manufactured by Micro Craft, Inc., Tullahoma, Tennessee. Orbital Sciences Corporation, Chandler, Arizona, built the Pegasus rocket booster used to launch the X-43 vehicles. For the Dryden research flights, the Pegasus rocket booster and attached X-43 will be air launched by Dryden's B-52 "Mothership." After release from the B-52, the booster will accelerate the X-43A vehicle to the established test conditions (Mach 7 to 10) at an altitude of approximately 100,000 feet where the X-43 will separate from the booster and fly under its own power and preprogrammed control. |
Photo Date |
December 1999 |
|
X-43A Vehicle During Ground
Photo Description |
The X-43A Hypersonic Experimental Vehicle, or "Hyper-X" is seen here undergoing ground testing at NASA's Dryden Flight Research Center, Edwards, California in December 1999. The X-43A was developed to research a dual-mode ramjet/scramjet propulsion system at speeds from Mach 7 up to Mach 10 (7 to 10 times the speed of sound, which varies with temperature and altitude). |
Project Description |
Hyper-X, the flight vehicle for which is designated as X-43A, is an experimental flight-research program seeking to demonstrate airframe-integrated, "air-breathing" engine technologies that promise to increase payload capacity for future vehicles, including hypersonic aircraft (faster than Mach 5) and reusable space launchers. This multiyear program is currently underway at NASA Dryden Flight Research Center, Edwards, California. The Hyper-X schedule calls for its first flight later this year (2000). Hyper-X is a joint program, with Dryden sharing responsibility with NASA's Langley Research Center, Hampton, Virginia. Dryden's primary role is to fly three unpiloted X-43A research vehicles to validate engine technologies and hypersonic design tools as well as the hypersonic test facility at Langley. Langley manages the program and leads the technology development effort. The Hyper-X Program seeks to significantly expand the speed boundaries of air-breathing propulsion by being the first aircraft to demonstrate an airframe-integrated, scramjet-powered free flight. Scramjets (supersonic-combustion ramjets) are ramjet engines in which the airflow through the whole engine remains supersonic. Scramjet technology is challenging because only limited testing can be performed in ground facilities. Long duration, full-scale testing requires flight research. Scramjet engines are air-breathing, capturing their oxygen from the atmosphere. Current spacecraft, such as the Space Shuttle, are rocket powered, so they must carry both fuel and oxygen for propulsion. Scramjet technology-based vehicles need to carry only fuel. By eliminating the need to carry oxygen, future hypersonic vehicles will be able to carry heavier payloads. Another unique aspect of the X-43A vehicle is the airframe integration. The body of the vehicle itself forms critical elements of the engine. The forebody acts as part of the intake for airflow and the aft section serves as the nozzle. The X-43A vehicles were manufactured by Micro Craft, Inc., Tullahoma, Tennessee. Orbital Sciences Corporation, Chandler, Arizona, built the Pegasus rocket booster used to launch the X-43 vehicles. For the Dryden research flights, the Pegasus rocket booster and attached X-43 will be air launched by Dryden's B-52 "Mothership." After release from the B-52, the booster will accelerate the X-43A vehicle to the established test conditions (Mach 7 to 10) at an altitude of approximately 100,000 feet where the X-43 will separate from the booster and fly under its own power and preprogrammed control. |
Photo Date |
December 1999 |
|
X-43A Vehicle During Ground
Photo Description |
The X-43A Hypersonic Experimental Vehicle, or "Hyper-X" is seen here undergoing ground testing at NASA's Dryden Flight Research Center, Edwards, California in December 1999. The X-43A was developed to research a dual-mode ramjet/scramjet propulsion system at speeds from Mach 7 up to Mach 10 (7 to 10 times the speed of sound, which varies with temperature and altitude). |
Project Description |
Hyper-X, the flight vehicle for which is designated as X-43A, is an experimental flight-research program seeking to demonstrate airframe-integrated, "air-breathing" engine technologies that promise to increase payload capacity for future vehicles, including hypersonic aircraft (faster than Mach 5) and reusable space launchers. This multiyear program is currently underway at NASA Dryden Flight Research Center, Edwards, California. The Hyper-X schedule calls for its first flight later this year (2000). Hyper-X is a joint program, with Dryden sharing responsibility with NASA's Langley Research Center, Hampton, Virginia. Dryden's primary role is to fly three unpiloted X-43A research vehicles to validate engine technologies and hypersonic design tools as well as the hypersonic test facility at Langley. Langley manages the program and leads the technology development effort. The Hyper-X Program seeks to significantly expand the speed boundaries of air-breathing propulsion by being the first aircraft to demonstrate an airframe-integrated, scramjet-powered free flight. Scramjets (supersonic-combustion ramjets) are ramjet engines in which the airflow through the whole engine remains supersonic. Scramjet technology is challenging because only limited testing can be performed in ground facilities. Long duration, full-scale testing requires flight research. Scramjet engines are air-breathing, capturing their oxygen from the atmosphere. Current spacecraft, such as the Space Shuttle, are rocket powered, so they must carry both fuel and oxygen for propulsion. Scramjet technology-based vehicles need to carry only fuel. By eliminating the need to carry oxygen, future hypersonic vehicles will be able to carry heavier payloads. Another unique aspect of the X-43A vehicle is the airframe integration. The body of the vehicle itself forms critical elements of the engine. The forebody acts as part of the intake for airflow and the aft section serves as the nozzle. The X-43A vehicles were manufactured by Micro Craft, Inc., Tullahoma, Tennessee. Orbital Sciences Corporation, Chandler, Arizona, built the Pegasus rocket booster used to launch the X-43 vehicles. For the Dryden research flights, the Pegasus rocket booster and attached X-43 will be air launched by Dryden's B-52 "Mothership." After release from the B-52, the booster will accelerate the X-43A vehicle to the established test conditions (Mach 7 to 10) at an altitude of approximately 100,000 feet where the X-43 will separate from the booster and fly under its own power and preprogrammed control. |
Photo Date |
December 1999 |
|
Hyper-X Research Vehicle - A
Photo Description |
This artist?s concept depicts the Hyper-X research vehicle riding on a booster rocket prior to being launched by the Dryden Flight Research Center's B-52 at about 40,000 feet. The X-43A was developed to flight test a dual-mode ramjet/scramjet propulsion system at speeds from Mach 7 up to Mach 10 (7 to 10 times the speed of sound, which varies with temperature and altitude). |
Project Description |
Hyper-X, the flight vehicle for which is designated as X-43A, is an experimental flight-research program seeking to demonstrate airframe-integrated, "air-breathing" engine technologies that promise to increase payload capacity for future vehicles, including hypersonic aircraft (faster than Mach 5) and reusable space launchers. This multiyear program is currently underway at NASA Dryden Flight Research Center, Edwards, California. The Hyper-X schedule calls for its first flight later this year (2000). Hyper-X is a joint program, with Dryden sharing responsibility with NASA's Langley Research Center, Hampton, Virginia. Dryden's primary role is to fly three unpiloted X-43A research vehicles to validate engine technologies and hypersonic design tools as well as the hypersonic test facility at Langley. Langley manages the program and leads the technology development effort. The Hyper-X Program seeks to significantly expand the speed boundaries of air-breathing propulsion by being the first aircraft to demonstrate an airframe-integrated, scramjet-powered free flight. Scramjets (supersonic-combustion ramjets) are ramjet engines in which the airflow through the whole engine remains supersonic. Scramjet technology is challenging because only limited testing can be performed in ground facilities. Long duration, full-scale testing requires flight research. Scramjet engines are air-breathing, capturing their oxygen from the atmosphere. Current spacecraft, such as the Space Shuttle, are rocket powered, so they must carry both fuel and oxygen for propulsion. Scramjet technology-based vehicles need to carry only fuel. By eliminating the need to carry oxygen, future hypersonic vehicles will be able to carry heavier payloads. Another unique aspect of the X-43A vehicle is the airframe integration. The body of the vehicle itself forms critical elements of the engine. The forebody acts as part of the intake for airflow and the aft section serves as the nozzle. The X-43A vehicles were manufactured by Micro Craft, Inc., Tullahoma, Tennessee. Orbital Sciences Corporation, Chandler, Arizona, built the Pegasus rocket booster used to launch the X-43 vehicles. For the Dryden research flights, the Pegasus rocket booster and attached X-43 will be air launched by Dryden's B-52 "Mothership." After release from the B-52, the booster will accelerate the X-43A vehicle to the established test conditions (Mach 7 to 10) at an altitude of approximately 100,000 feet where the X-43 will separate from the booster and fly under its own power and preprogrammed control. |
Photo Date |
1997 |
|
F-111 TACT research flight o
The Road to Apollo
Even before the Space Task G
3/30/09
Description |
Even before the Space Task Group was formally organized, Langley had begun to develop the concept of the "Little Joe" test vehicle that became the workhorse of the nation's initial humans-in-space program -- Mercury. Little Joe, a solid fuel rocket, carried instrumented payloads to various altitudes and allowed engineers to check the operation of the Mercury capsule escape rocket and recovery systems. Here Langley technicians construct the Little Joe capsules in-house in Langley's shops. Credit: NASA |
Date |
3/30/09 |
|
Photo Description |
Joel Sitz is the project manager of the X-43 experimental aircraft [ http://www.dfrc.nasa.gov/Gallery/Photo/X-43A/index.html ] at NASA's Dryden Flight Research Center, Edwards, California, a position he has held since July 1998. Sitz is responsible for the overall flight research element of the Hyper-X Program, managed by the NASA Langley Research Center, Hampton, Va. The X-43A vehicle will feature the first free flight of an airframe-integrated, hypersonic Supersonic Combustion RamJet (SCRAMJET) engine. Before assuming his present assignment, Sitz was deputy program manager at Dryden for NASA?s Aviation Safety Program from 1997 to 1998. He was also the project manager of the F-18 Systems Research Aircraft (SRA) and the L-1011 Adaptive Performance Optimization (APO) Project. His responsibilities included the development and flight evaluation of several advanced aircraft sensors and systems technologies that will be used to improve both the safety and performance of future military and commercial transport aircraft. Previous to joining NASA in 1989 as an aerospace engineer, Sitz was employed by Honeywell Military Avionics Division. At NASA he became a software systems engineer on the X-29 Forward Swept Wing Project, responsible for real-time flight control software design, development and test. At Dryden, Sitz has developed and performed research in advanced automated test tools to support flight control system validation for flight research projects including the X-29, F-18 High Angle of Attack and X-31 flight research programs. He was the deputy project manager for the F-16XL #2 Supersonic Laminar Flow Control Project. He was also the project manager responsible for transfer of Dryden business system operations from NASA Ames Research Center, Moffett Field, Calif., to NASA Marshall Space Flight Center, Huntsville, Ala., when Dryden became an independent NASA center in 1994. As a member of Dryden?s Procedures and Policies Committee from 1990 to 1997, Sitz was responsible for updating Dryden?s Basic Operations Manual. Sitz graduated from the University of North Dakota in 1982 with a bachelor of science degree in computer science. He received a master of science degree in engineering management in 1989 from Golden Gate University of San Francisco, Calif. |
Project Description |
unknown |
Photo Date |
March 19, 2004 |
|
Working for Quieter Airplane
Gold-colored foam wedges shi
1/7/09
Description |
Gold-colored foam wedges shield test subjects from outside noises during an acoustics test at NASA's Langley Research Center in Hampton, Va. NASA researchers study people's perception of aircraft sounds, especially the role of rattle noises and vibration. They use this information to help design quieter aircraft. Credit: NASA Langley/Sean Smith |
Date |
1/7/09 |
|
The Road to Apollo
A full-scale model of the Me
3/16/09
Description |
A full-scale model of the Mercury capsule was tested in the Langley 30- by 60-Foot Full-Scale Wind Tunnel. Managed at Langley Research Center, the objectives of the Mercury program were quite specific -- to orbit a crewed spacecraft around the Earth, to investigate the ability of humans to function in space and to recover both human and spacecraft safely. Project Mercury accomplished the first orbital flight made by an American, astronaut John Glenn. Credit: NASA |
Date |
3/16/09 |
|
Dance Across
Mysterious chalkings have be
4/28/09
Description |
Mysterious chalkings have been reported throughout NASA Langley Research Center. The puzzling messages appeared overnight and urge employees to take bizarre actions, such as smile, dance through crosswalks and skip to work. Safety officials tested the chalk and have confirmed that it presents no problem to employees. Langley spokesperson Marny Skora says management encourages employees to take risks, noting that as one chalking indicates, "Every noble work is at first impossible." Credit: NASA/Sean Smith |
Date |
4/28/09 |
|
Eschew Obfuscation
Mysterious chalkings have be
4/28/09
Description |
Mysterious chalkings have been reported throughout NASA Langley Research Center. The puzzling messages appeared overnight and urge employees to take bizarre actions, such as smile, dance through crosswalks and skip to work. Safety officials tested the chalk and have confirmed that it presents no problem to employees. Langley spokesperson Marny Skora says management encourages employees to take risks, noting that as one chalking indicates, "Every noble work is at first impossible." Credit: NASA/Sean Smith |
Date |
4/28/09 |
|
Baby You Light My Fire
Mysterious chalkings have be
4/28/09
Description |
Mysterious chalkings have been reported throughout NASA Langley Research Center. The puzzling messages appeared overnight and urge employees to take bizarre actions, such as smile, dance through crosswalks and skip to work. Safety officials tested the chalk and have confirmed that it presents no problem to employees. Langley spokesperson Marny Skora says management encourages employees to take risks, noting that as one chalking indicates, "Every noble work is at first impossible." Credit: NASA/Sean Smith |
Date |
4/28/09 |
|
Life is Good!
Mysterious chalkings have be
4/28/09
Description |
Mysterious chalkings have been reported throughout NASA Langley Research Center. The puzzling messages appeared overnight and urge employees to take bizarre actions, such as smile, dance through crosswalks and skip to work. Safety officials tested the chalk and have confirmed that it presents no problem to employees. Langley spokesperson Marny Skora says management encourages employees to take risks, noting that as one chalking indicates, "Every noble work is at first impossible." Credit: NASA/Sean Smith |
Date |
4/28/09 |
|
Skip to the Office
Mysterious chalkings have be
4/28/09
Description |
Mysterious chalkings have been reported throughout NASA Langley Research Center. The puzzling messages appeared overnight and urge employees to take bizarre actions, such as smile, dance through crosswalks and skip to work. Safety officials tested the chalk and have confirmed that it presents no problem to employees. Langley spokesperson Marny Skora says management encourages employees to take risks, noting that as one chalking indicates, "Every noble work is at first impossible." Credit: NASA/Sean Smith |
Date |
4/28/09 |
|
Teachers Rule!
Mysterious chalkings have be
4/28/09
Description |
Mysterious chalkings have been reported throughout NASA Langley Research Center. The puzzling messages appeared overnight and urge employees to take bizarre actions, such as smile, dance through crosswalks and skip to work. Safety officials tested the chalk and have confirmed that it presents no problem to employees. Langley spokesperson Marny Skora says management encourages employees to take risks, noting that as one chalking indicates, "Every noble work is at first impossible." Credit: NASA/Sean Smith |
Date |
4/28/09 |
|
United We Serve -- Denise Li
Denise Lineberry is an edito
9/4/09
Description |
Denise Lineberry is an editor for NASA Langley's newspaper. She also uses her expertise to fight illiteracy in Hampton Roads. |
Date |
9/4/09 |
|
The Road to Apollo
As project Mercury began in
3/16/09
Description |
As project Mercury began in the late 1950s, Langley was thrust full force into the national spotlight with the arrival in Hampton of the original seven astronauts. Under the tutelage of the Space Task Group, (from left front row) Virgil "Gus" Grissom, Scott Carpenter, Donald "Deke" Slayton, Gordon Cooper, (back row) Alan Shepard, Walter Schirra and John Glenn were trained at Langley to operate the space machines that would thrust them beyond the protective environment of Earth's atmosphere. Credit: NASA |
Date |
3/16/09 |
|
EarthFest Podcasts
Kate Coleman, daughter of Li
5/13/08
Description |
Kate Coleman, daughter of Lisa Coleman of the Science Directorate, watches and listens to science videos and podcasts at EarthFest. Credit: NASA/Sean Smith |
Date |
5/13/08 |
|
NASA Connect - Measurement,
NASA Connect Video containin
10/1/00
Description |
NASA Connect Video containing five segments as described below. NASA Connect segment exploring how NASA scientests use measurement, ratios, and graphing to help test aircraft at the Impact Dynamics Research Facility. NASA Connect segment involving students in a web-based activity called Edutour sponsored by Nauticus. The edutour is a digital tour of the NASA Langley Aircraft Landing Dynamics Facility. NASA Connect segment explaining NASA Langley's Aircraft Landing Dynamics Facility, or ALDF. The video explores how scientists are using math and technology to test tires, wheels, and brakes. NASA Connect segment involving students in a hands-on activity that simulates the research from the ALDF test track. The students use an Effervescent Non-combustible Dragster to test different ratios of water and effervescent tablets then students graph the data. NASA Connect segment exploring the NASA Langley facility. The video also explains the history of NASA Langley and how scientists there use measurement, ratios, and graphing. |
Date |
10/1/00 |
|
Ask A Scientist
Scientists from the Science
5/13/08
Description |
Scientists from the Science Directorate at NASA's Langley Research Center, including Marty Mlynczak, Bruce Doddridge and Lin Chambers, participated in a series of "Ask a Scientist" panels for the public at EarthFest. Colleagues from the Virginia Institute for Marine Science and from the College of William and Mary also participated as panelists. The space also served as a gallery for Earth art, photographs and data images of our home planet from space. Credit: NASA/Sean Smith |
Date |
5/13/08 |
|
Crew Module, Launch Abort Sy
NASA is a step closer to the
1/26/09
Description |
NASA is a step closer to the first flight test of its back-to-the-moon rocket design with the completion of key Ares I-X rocket hardware elements at NASA's Langley Research Center, in Hampton, Va. Credit: NASA/Sean Smith |
Date |
1/26/09 |
|
The Road to Apollo
Almost 40 years have passed
2/13/09
Description |
Almost 40 years have passed since July 20, 1969, when the lunar module "Eagle" carrying Apollo 11 astronauts Neil Armstrong and Buzz Aldrin gingerly made its way down to the Sea of Tranquility, landing humans on the moon for the first time. "From launch to splashdown, there was no aspect of the Apollo mission that scientists, engineers and technicians at NASA's Langley Research Center had not helped to develop in one way or another," said historian James R. Hansen, author of Spaceflight Revolution. This weekly series of photographs will highlight some of the Hampton center's contributions on "The road to Apollo." Credit: NASA |
Date |
2/13/09 |
|
NASA Reinstalls Main Mirror
Engineers and technicians fr
10/28/08
Description |
Engineers and technicians from NASA, the German Space Agency and the Deutsches SOFIA Institut recently reinstalled the German-built primary mirror assembly into NASA's Stratospheric Observatory for Infrared Astronomy, or SOFIA, airborne observatory. Technicians removed the glass mirror from the modified 747SP observatory in April 2008 and transported it to NASA's Ames Research Center, Moffett Field, Calif., where it received its reflective aluminum coating in a vacuum chamber in June 2008. The coating, five one-millionths of an inch thick, will be reapplied as necessary during the 20-year life of the program. "We had completed system tests of our mirror coater but this is the first time we've actually coated SOFIA's mirror. The team and equipment performed flawlessly and the results are magnificent," says Ed Austin, SOFIA science project manager at Ames. The mirror assembly was transported back to NASA's Dryden Aircraft Operations Facility in Palmdale, Calif., mid-September and reinstalled Oct. 8. "The reinstallation of the mirror is a significant program milestone on the path to science observations with the SOFIA observatory in the summer of 2009," said Bob Meyer, SOFIA program manager at NASA's Dryden Flight Research Center, Edwards, Calif. › Read more Photo Description A technician guides SOFIA's primary mirror assembly into the aircraft's telescope cavity completing the mirror reinstallation following its initial coating. October 8, 2008 NASA Photo / Carla Thomas ED08-0262-54 |
Date |
10/28/08 |
|
Some NACA Muroc personnel wi
Photo Description |
The late 1940s saw increased flight activity, and more women computers were needed at the NACA Muroc Flight Test Unit than the ones who had originally arrived in 1946. A call went out to the NACA Langley, Lewis, and Ames laboratories for more women computers. Pictured in this photograph with the Snowman are some of the women computers who responded to the call for help in 1948 along with Roxanah, Emily, Dorothy, who were already here. Standing left to right: Mary (Tut) Hedgepeth, from Langley, Lilly Ann Bajus, Lewis, Roxanah Yancey, Emily Stephens, Jane Collons (Procurement), Leona Corbett (Personnel), Angel Dunn, Langley. Kneeling left to right: Dorothy (Dottie) Crawford Roth, Lewis, Dorothy Clift Hughes, and Gertrude (Trudy) Wilken Valentine, Lewis. |
Project Description |
In National Advisory Committee for Aeronautics (NACA) terminology of 1946, computers were employees who performed laborious and time-consuming mathematical calculations and data reduction from long strips of records generated by onboard aircraft instrumentation. Virtually without exception, computers were female, at least part of the rationale seems to have been the notion that the work was long and tedious, and men were not thought to have the patience to do it. Though equipment changed over the years and most computers eventually found themselves programming and operating electronic computers, as well as doing other data processing tasks, being a computer initially meant long hours with a slide rule, hunched over illuminated light boxes measuring line traces from grainy and obscure strips of oscillograph film. Computers suffered terrible eyestrain, and those who didn't begin by wearing glasses did so after a few years. But they were initially essential employees at the Muroc Flight Test Unit and NACA High-Speed Flight Research Station, taking the oscillograph flight records and "reducing" the data on them to make them useful to research engineers, who analyzed the data. |
Photo Date |
15 Nov 1949 |
|
X-43A Undergoing Controlled
Photo Description |
The X-43A Hypersonic Experimental (Hyper-X) Vehicle hangs suspended in the cavernous Benefield Aenechoic Facility at Edwards Air Force Base during radio frequency tests in January 2000. |
Project Description |
Hyper-X, the flight vehicle for which is designated as X-43A, is an experimental flight-research program seeking to demonstrate airframe-integrated, "air-breathing" engine technologies that promise to increase payload capacity for future vehicles, including hypersonic aircraft (faster than Mach 5) and reusable space launchers. This multiyear program is currently underway at NASA Dryden Flight Research Center, Edwards, California. The Hyper-X schedule calls for its first flight later this year (2000). Hyper-X is a joint program, with Dryden sharing responsibility with NASA's Langley Research Center, Hampton, Virginia. Dryden's primary role is to fly three unpiloted X-43A research vehicles to validate engine technologies and hypersonic design tools as well as the hypersonic test facility at Langley. Langley manages the program and leads the technology development effort. The Hyper-X Program seeks to significantly expand the speed boundaries of air-breathing propulsion by being the first aircraft to demonstrate an airframe-integrated, scramjet-powered free flight. Scramjets (supersonic-combustion ramjets) are ramjet engines in which the airflow through the whole engine remains supersonic. Scramjet technology is challenging because only limited testing can be performed in ground facilities. Long duration, full-scale testing requires flight research. Scramjet engines are air-breathing, capturing their oxygen from the atmosphere. Current spacecraft, such as the Space Shuttle, are rocket powered, so they must carry both fuel and oxygen for propulsion. Scramjet technology-based vehicles need to carry only fuel. By eliminating the need to carry oxygen, future hypersonic vehicles will be able to carry heavier payloads. Another unique aspect of the X-43A vehicle is the airframe integration. The body of the vehicle itself forms critical elements of the engine. The forebody acts as part of the intake for airflow and the aft section serves as the nozzle. The X-43A vehicles were manufactured by Micro Craft, Inc., Tullahoma, Tennessee. Orbital Sciences Corporation, Chandler, Arizona, built the Pegasus rocket booster used to launch the X-43 vehicles. For the Dryden research flights, the Pegasus rocket booster and attached X-43 will be air launched by Dryden's B-52 "Mothership." After release from the B-52, the booster will accelerate the X-43A vehicle to the established test conditions (Mach 7 to 10) at an altitude of approximately 100,000 feet where the X-43 will separate from the booster and fly under its own power and preprogrammed control. |
Photo Date |
January 2000 |
|
X-43A Undergoing Controlled
Photo Description |
The X-43A Hypersonic Experimental (Hyper-X) Vehicle hangs suspended in the cavernous Benefield Aenechoic Facility at Edwards Air Force Base during radio frequency tests in January 2000. |
Project Description |
Hyper-X, the flight vehicle for which is designated as X-43A, is an experimental flight-research program seeking to demonstrate airframe-integrated, "air-breathing" engine technologies that promise to increase payload capacity for future vehicles, including hypersonic aircraft (faster than Mach 5) and reusable space launchers. This multiyear program is currently underway at NASA Dryden Flight Research Center, Edwards, California. The Hyper-X schedule calls for its first flight later this year (2000). Hyper-X is a joint program, with Dryden sharing responsibility with NASA's Langley Research Center, Hampton, Virginia. Dryden's primary role is to fly three unpiloted X-43A research vehicles to validate engine technologies and hypersonic design tools as well as the hypersonic test facility at Langley. Langley manages the program and leads the technology development effort. The Hyper-X Program seeks to significantly expand the speed boundaries of air-breathing propulsion by being the first aircraft to demonstrate an airframe-integrated, scramjet-powered free flight. Scramjets (supersonic-combustion ramjets) are ramjet engines in which the airflow through the whole engine remains supersonic. Scramjet technology is challenging because only limited testing can be performed in ground facilities. Long duration, full-scale testing requires flight research. Scramjet engines are air-breathing, capturing their oxygen from the atmosphere. Current spacecraft, such as the Space Shuttle, are rocket powered, so they must carry both fuel and oxygen for propulsion. Scramjet technology-based vehicles need to carry only fuel. By eliminating the need to carry oxygen, future hypersonic vehicles will be able to carry heavier payloads. Another unique aspect of the X-43A vehicle is the airframe integration. The body of the vehicle itself forms critical elements of the engine. The forebody acts as part of the intake for airflow and the aft section serves as the nozzle. The X-43A vehicles were manufactured by Micro Craft, Inc., Tullahoma, Tennessee. Orbital Sciences Corporation, Chandler, Arizona, built the Pegasus rocket booster used to launch the X-43 vehicles. For the Dryden research flights, the Pegasus rocket booster and attached X-43 will be air launched by Dryden's B-52 "Mothership." After release from the B-52, the booster will accelerate the X-43A vehicle to the established test conditions (Mach 7 to 10) at an altitude of approximately 100,000 feet where the X-43 will separate from the booster and fly under its own power and preprogrammed control. |
Photo Date |
January 2000 |
|
X-43A Undergoing Controlled
Photo Description |
The X-43A Hypersonic Experimental (Hyper-X) Vehicle hangs suspended in the cavernous Benefield Aenechoic Facility at Edwards Air Force Base during radio frequency tests in January 2000. |
Project Description |
Hyper-X, the flight vehicle for which is designated as X-43A, is an experimental flight-research program seeking to demonstrate airframe-integrated, "air-breathing" engine technologies that promise to increase payload capacity for future vehicles, including hypersonic aircraft (faster than Mach 5) and reusable space launchers. This multiyear program is currently underway at NASA Dryden Flight Research Center, Edwards, California. The Hyper-X schedule calls for its first flight later this year (2000). Hyper-X is a joint program, with Dryden sharing responsibility with NASA's Langley Research Center, Hampton, Virginia. Dryden's primary role is to fly three unpiloted X-43A research vehicles to validate engine technologies and hypersonic design tools as well as the hypersonic test facility at Langley. Langley manages the program and leads the technology development effort. The Hyper-X Program seeks to significantly expand the speed boundaries of air-breathing propulsion by being the first aircraft to demonstrate an airframe-integrated, scramjet-powered free flight. Scramjets (supersonic-combustion ramjets) are ramjet engines in which the airflow through the whole engine remains supersonic. Scramjet technology is challenging because only limited testing can be performed in ground facilities. Long duration, full-scale testing requires flight research. Scramjet engines are air-breathing, capturing their oxygen from the atmosphere. Current spacecraft, such as the Space Shuttle, are rocket powered, so they must carry both fuel and oxygen for propulsion. Scramjet technology-based vehicles need to carry only fuel. By eliminating the need to carry oxygen, future hypersonic vehicles will be able to carry heavier payloads. Another unique aspect of the X-43A vehicle is the airframe integration. The body of the vehicle itself forms critical elements of the engine. The forebody acts as part of the intake for airflow and the aft section serves as the nozzle. The X-43A vehicles were manufactured by Micro Craft, Inc., Tullahoma, Tennessee. Orbital Sciences Corporation, Chandler, Arizona, built the Pegasus rocket booster used to launch the X-43 vehicles. For the Dryden research flights, the Pegasus rocket booster and attached X-43 will be air launched by Dryden's B-52 "Mothership." After release from the B-52, the booster will accelerate the X-43A vehicle to the established test conditions (Mach 7 to 10) at an altitude of approximately 100,000 feet where the X-43 will separate from the booster and fly under its own power and preprogrammed control. |
Photo Date |
January 2000 |
|
X-43A Undergoing Controlled
Photo Description |
The X-43A Hypersonic Experimental (Hyper-X) Vehicle hangs suspended in the cavernous Benefield Aenechoic Facility at Edwards Air Force Base during radio frequency tests in January 2000. |
Project Description |
Hyper-X, the flight vehicle for which is designated as X-43A, is an experimental flight-research program seeking to demonstrate airframe-integrated, "air-breathing" engine technologies that promise to increase payload capacity for future vehicles, including hypersonic aircraft (faster than Mach 5) and reusable space launchers. This multiyear program is currently underway at NASA Dryden Flight Research Center, Edwards, California. The Hyper-X schedule calls for its first flight later this year (2000). Hyper-X is a joint program, with Dryden sharing responsibility with NASA's Langley Research Center, Hampton, Virginia. Dryden's primary role is to fly three unpiloted X-43A research vehicles to validate engine technologies and hypersonic design tools as well as the hypersonic test facility at Langley. Langley manages the program and leads the technology development effort. The Hyper-X Program seeks to significantly expand the speed boundaries of air-breathing propulsion by being the first aircraft to demonstrate an airframe-integrated, scramjet-powered free flight. Scramjets (supersonic-combustion ramjets) are ramjet engines in which the airflow through the whole engine remains supersonic. Scramjet technology is challenging because only limited testing can be performed in ground facilities. Long duration, full-scale testing requires flight research. Scramjet engines are air-breathing, capturing their oxygen from the atmosphere. Current spacecraft, such as the Space Shuttle, are rocket powered, so they must carry both fuel and oxygen for propulsion. Scramjet technology-based vehicles need to carry only fuel. By eliminating the need to carry oxygen, future hypersonic vehicles will be able to carry heavier payloads. Another unique aspect of the X-43A vehicle is the airframe integration. The body of the vehicle itself forms critical elements of the engine. The forebody acts as part of the intake for airflow and the aft section serves as the nozzle. The X-43A vehicles were manufactured by Micro Craft, Inc., Tullahoma, Tennessee. Orbital Sciences Corporation, Chandler, Arizona, built the Pegasus rocket booster used to launch the X-43 vehicles. For the Dryden research flights, the Pegasus rocket booster and attached X-43 will be air launched by Dryden's B-52 "Mothership." After release from the B-52, the booster will accelerate the X-43A vehicle to the established test conditions (Mach 7 to 10) at an altitude of approximately 100,000 feet where the X-43 will separate from the booster and fly under its own power and preprogrammed control. |
Photo Date |
January 2000 |
|
Hyper-X Vehicle Model - Side
Photo Description |
A side-view of an early desk-top model of NASA's X-43A "Hyper-X," or Hypersonic Experimental Vehicle, which has been developed to flight test a dual-mode ramjet/scramjet propulsion system at speeds from Mach 7 up to Mach 10 (7 to 10 times the speed of sound, which varies with temperature and altitude). |
Project Description |
Hyper-X, the flight vehicle for which is designated as X-43A, is an experimental flight-research program seeking to demonstrate airframe-integrated, "air-breathing" engine technologies that promise to increase payload capacity for future vehicles, including hypersonic aircraft (faster than Mach 5) and reusable space launchers. This multiyear program is currently underway at NASA Dryden Flight Research Center, Edwards, California. The Hyper-X schedule calls for its first flight later this year (2000). Hyper-X is a joint program, with Dryden sharing responsibility with NASA?s Langley Research Center, Hampton, Virginia. Dryden?s primary role is to fly three unpiloted X-43A research vehicles to validate engine technologies and hypersonic design tools as well as the hypersonic test facility at Langley. Langley manages the program and leads the technology development effort. The Hyper-X Program seeks to significantly expand the speed boundaries of air-breathing propulsion by being the first aircraft to demonstrate an airframe-integrated, scramjet-powered free flight. Scramjets (supersonic-combustion ramjets) are ramjet engines in which the airflow through the whole engine remains supersonic. Scramjet technology is challenging because only limited testing can be performed in ground facilities. Long duration, full-scale testing requires flight research. Scramjet engines are air-breathing, capturing their oxygen from the atmosphere. Current spacecraft, such as the Space Shuttle, are rocket powered, so they must carry both fuel and oxygen for propulsion. Scramjet technology-based vehicles need to carry only fuel. By eliminating the need to carry oxygen, future hypersonic vehicles will be able to carry heavier payloads. Another unique aspect of the X-43A vehicle is the airframe integration. The body of the vehicle itself forms critical elements of the engine. The forebody acts as part of the intake for airflow and the aft section serves as the nozzle. The X-43A vehicles were manufactured by Micro Craft, Inc., Tullahoma, Tennessee. Orbital Sciences Corporation, Chandler, Arizona, built the Pegasus rocket booster used to launch the X-43 vehicles. For the Dryden research flights, the Pegasus rocket booster and attached X-43 will be air launched by Dryden?s B-52 "Mothership." After release from the B-52, the booster will accelerate the X-43A vehicle to the established test conditions (Mach 7 to 10) at an altitude of approximately 100,000 feet where the X-43 will separate from the booster and fly under its own power and preprogrammed control. |
Photo Date |
August 1996 |
|
Hyper-X Vehicle Model - Side
Photo Description |
Sleek lines are apparent in this side-view of an early desk-top model of NASA's X-43A "Hyper-X," or Hypersonic Experimental Vehicle, which has been developed to flight test a dual-mode ramjet/scramjet propulsion system at speeds from Mach 7 up to Mach 10 (7 to 10 times the speed of sound, which varies with temperature and altitude). |
Project Description |
Hyper-X, the flight vehicle for which is designated as X-43A, is an experimental flight-research program seeking to demonstrate airframe-integrated, "air-breathing" engine technologies that promise to increase payload capacity for future vehicles, including hypersonic aircraft (faster than Mach 5) and reusable space launchers. This multiyear program is currently underway at NASA Dryden Flight Research Center, Edwards, California. The Hyper-X schedule calls for its first flight later this year (2000). Hyper-X is a joint program, with Dryden sharing responsibility with NASA?s Langley Research Center, Hampton, Virginia. Dryden?s primary role is to fly three unpiloted X-43A research vehicles to validate engine technologies and hypersonic design tools as well as the hypersonic test facility at Langley. Langley manages the program and leads the technology development effort. The Hyper-X Program seeks to significantly expand the speed boundaries of air-breathing propulsion by being the first aircraft to demonstrate an airframe-integrated, scramjet-powered free flight. Scramjets (supersonic-combustion ramjets) are ramjet engines in which the airflow through the whole engine remains supersonic. Scramjet technology is challenging because only limited testing can be performed in ground facilities. Long duration, full-scale testing requires flight research. Scramjet engines are air-breathing, capturing their oxygen from the atmosphere. Current spacecraft, such as the Space Shuttle, are rocket powered, so they must carry both fuel and oxygen for propulsion. Scramjet technology-based vehicles need to carry only fuel. By eliminating the need to carry oxygen, future hypersonic vehicles will be able to carry heavier payloads. Another unique aspect of the X-43A vehicle is the airframe integration. The body of the vehicle itself forms critical elements of the engine. The forebody acts as part of the intake for airflow and the aft section serves as the nozzle. The X-43A vehicles were manufactured by Micro Craft, Inc., Tullahoma, Tennessee. Orbital Sciences Corporation, Chandler, Arizona, built the Pegasus rocket booster used to launch the X-43 vehicles. For the Dryden research flights, the Pegasus rocket booster and attached X-43 will be air launched by Dryden?s B-52 "Mothership." After release from the B-52, the booster will accelerate the X-43A vehicle to the established test conditions (Mach 7 to 10) at an altitude of approximately 100,000 feet where the X-43 will separate from the booster and fly under its own power and preprogrammed control. |
Photo Date |
August 1996 |
|
Hyper-X Vehicle Model - Top
Photo Description |
This aft-quarter model view of NASA's X-43A "Hyper-X" or Hypersonic Experimental Vehicle shows its sleek, geometric design. The X-43A was developed to flight test a dual-mode ramjet/scramjet propulsion system at speeds from Mach 7 up to Mach 10 (7 to 10 times the speed of sound, which varies with temperature and altitude). |
Project Description |
Hyper-X, the flight vehicle for which is designated as X-43A, is an experimental flight-research program seeking to demonstrate airframe-integrated, "air-breathing" engine technologies that promise to increase payload capacity for future vehicles, including hypersonic aircraft (faster than Mach 5) and reusable space launchers. This multiyear program is currently underway at NASA Dryden Flight Research Center, Edwards, California. The Hyper-X schedule calls for its first flight later this year (2000). Hyper-X is a joint program, with Dryden sharing responsibility with NASA's Langley Research Center, Hampton, Virginia. Dryden's primary role is to fly three unpiloted X-43A research vehicles to validate engine technologies and hypersonic design tools as well as the hypersonic test facility at Langley. Langley manages the program and leads the technology development effort. The Hyper-X Program seeks to significantly expand the speed boundaries of air-breathing propulsion by being the first aircraft to demonstrate an airframe-integrated, scramjet-powered free flight. Scramjets (supersonic-combustion ramjets) are ramjet engines in which the airflow through the whole engine remains supersonic. Scramjet technology is challenging because only limited testing can be performed in ground facilities. Long duration, full-scale testing requires flight research. Scramjet engines are air-breathing, capturing their oxygen from the atmosphere. Current spacecraft, such as the Space Shuttle, are rocket powered, so they must carry both fuel and oxygen for propulsion. Scramjet technology-based vehicles need to carry only fuel. By eliminating the need to carry oxygen, future hypersonic vehicles will be able to carry heavier payloads. Another unique aspect of the X-43A vehicle is the airframe integration. The body of the vehicle itself forms critical elements of the engine. The forebody acts as part of the intake for airflow and the aft section serves as the nozzle. The X-43A vehicles were manufactured by Micro Craft, Inc., Tullahoma, Tennessee. Orbital Sciences Corporation, Chandler, Arizona, built the Pegasus rocket booster used to launch the X-43 vehicles. For the Dryden research flights, the Pegasus rocket booster and attached X-43 will be air launched by Dryden's B-52 "Mothership." After release from the B-52, the booster will accelerate the X-43A vehicle to the established test conditions (Mach 7 to 10) at an altitude of approximately 100,000 feet where the X-43 will separate from the booster and fly under its own power and preprogrammed control. |
Photo Date |
August 1996 |
|
Hyper-X Vehicle Model - Fron
Photo Description |
A front view of an early desk-top model of NASA's X-43A "Hyper-X," or Hypersonic Experimental Vehicle, which has been developed to flight test a dual-mode ramjet/scramjet propulsion system at speeds from Mach 7 up to Mach 10 (7 to 10 times the speed of sound, which varies with temperature and altitude). |
Project Description |
Hyper-X, the flight vehicle for which is designated as X-43A, is an experimental flight-research program seeking to demonstrate airframe-integrated, "air-breathing" engine technologies that promise to increase payload capacity for future vehicles, including hypersonic aircraft (faster than Mach 5) and reusable space launchers. This multiyear program is currently underway at NASA Dryden Flight Research Center, Edwards, California. The Hyper-X schedule calls for its first flight later this year (2000). Hyper-X is a joint program, with Dryden sharing responsibility with NASA's Langley Research Center, Hampton, Virginia. Dryden's primary role is to fly three unpiloted X-43A research vehicles to validate engine technologies and hypersonic design tools as well as the hypersonic test facility at Langley. Langley manages the program and leads the technology development effort. The Hyper-X Program seeks to significantly expand the speed boundaries of air-breathing propulsion by being the first aircraft to demonstrate an airframe-integrated, scramjet-powered free flight. Scramjets (supersonic-combustion ramjets) are ramjet engines in which the airflow through the whole engine remains supersonic. Scramjet technology is challenging because only limited testing can be performed in ground facilities. Long duration, full-scale testing requires flight research. Scramjet engines are air-breathing, capturing their oxygen from the atmosphere. Current spacecraft, such as the Space Shuttle, are rocket powered, so they must carry both fuel and oxygen for propulsion. Scramjet technology-based vehicles need to carry only fuel. By eliminating the need to carry oxygen, future hypersonic vehicles will be able to carry heavier payloads. Another unique aspect of the X-43A vehicle is the airframe integration. The body of the vehicle itself forms critical elements of the engine. The forebody acts as part of the intake for airflow and the aft section serves as the nozzle. The X-43A vehicles were manufactured by Micro Craft, Inc., Tullahoma, Tennessee. Orbital Sciences Corporation, Chandler, Arizona, built the Pegasus rocket booster used to launch the X-43 vehicles. For the Dryden research flights, the Pegasus rocket booster and attached X-43 will be air launched by Dryden's B-52 "Mothership." After release from the B-52, the booster will accelerate the X-43A vehicle to the established test conditions (Mach 7 to 10) at an altitude of approximately 100,000 feet where the X-43 will separate from the booster and fly under its own power and preprogrammed control. |
Photo Date |
August 1996 |
|
Hyper-X Vehicle Model - Top
Photo Description |
A top front view of an early desk-top model of NASA's X-43A "Hyper-X," or Hypersonic Experimental Vehicle, developed to flight test a dual-mode ramjet/scramjet propulsion system at speeds from Mach 7 up to Mach 10 (7 to 10 times the speed of sound, which varies with temperature and altitude). |
Project Description |
Hyper-X, the flight vehicle for which is designated as X-43A, is an experimental flight-research program seeking to demonstrate airframe-integrated, "air-breathing" engine technologies that promise to increase payload capacity for future vehicles, including hypersonic aircraft (faster than Mach 5) and reusable space launchers. This multiyear program is currently underway at NASA Dryden Flight Research Center, Edwards, California. The Hyper-X schedule calls for its first flight later this year (2000). Hyper-X is a joint program, with Dryden sharing responsibility with NASA's Langley Research Center, Hampton, Virginia. Dryden's primary role is to fly three unpiloted X-43A research vehicles to validate engine technologies and hypersonic design tools as well as the hypersonic test facility at Langley. Langley manages the program and leads the technology development effort. The Hyper-X Program seeks to significantly expand the speed boundaries of air-breathing propulsion by being the first aircraft to demonstrate an airframe-integrated, scramjet-powered free flight. Scramjets (supersonic-combustion ramjets) are ramjet engines in which the airflow through the whole engine remains supersonic. Scramjet technology is challenging because only limited testing can be performed in ground facilities. Long duration, full-scale testing requires flight research. Scramjet engines are air-breathing, capturing their oxygen from the atmosphere. Current spacecraft, such as the Space Shuttle, are rocket powered, so they must carry both fuel and oxygen for propulsion. Scramjet technology-based vehicles need to carry only fuel. By eliminating the need to carry oxygen, future hypersonic vehicles will be able to carry heavier payloads. Another unique aspect of the X-43A vehicle is the airframe integration. The body of the vehicle itself forms critical elements of the engine. The forebody acts as part of the intake for airflow and the aft section serves as the nozzle. The X-43A vehicles were manufactured by Micro Craft, Inc., Tullahoma, Tennessee. Orbital Sciences Corporation, Chandler, Arizona, built the Pegasus rocket booster used to launch the X-43 vehicles. For the Dryden research flights, the Pegasus rocket booster and attached X-43 will be air launched by Dryden's B-52 "Mothership." After release from the B-52, the booster will accelerate the X-43A vehicle to the established test conditions (Mach 7 to 10) at an altitude of approximately 100,000 feet where the X-43 will separate from the booster and fly under its own power and preprogrammed control. |
Photo Date |
August 1996 |
|
Pegasus Rocket Booster Being
Photo Description |
Technicians prepare a Pegasus rocket booster for flight tests with the X-43A "Hypersonic Experimental Vehicle," or "Hyper-X." The X-43A, which will be attached to the Pegasus booster and drop launched from NASA's B-52 mothership, was developed to research dual-mode ramjet/scramjet propulsion system at speeds from Mach 7 up to Mach 10 (7 to 10 times the speed of sound, which varies with temperature and altitude). |
Project Description |
Hyper-X, the flight vehicle for which is designated as X-43A, is an experimental flight-research program seeking to demonstrate airframe-integrated, "air-breathing" engine technologies that promise to increase payload capacity for future vehicles, including hypersonic aircraft (faster than Mach 5) and reusable space launchers. This multiyear program is currently underway at NASA Dryden Flight Research Center, Edwards, California. The Hyper-X schedule calls for its first flight later this year (2000). Hyper-X is a joint program, with Dryden sharing responsibility with NASA's Langley Research Center, Hampton, Virginia. Dryden's primary role is to fly three unpiloted X-43A research vehicles to validate engine technologies and hypersonic design tools as well as the hypersonic test facility at Langley. Langley manages the program and leads the technology development effort. The Hyper-X Program seeks to significantly expand the speed boundaries of air-breathing propulsion by being the first aircraft to demonstrate an airframe-integrated, scramjet-powered free flight. Scramjets (supersonic-combustion ramjets) are ramjet engines in which the airflow through the whole engine remains supersonic. Scramjet technology is challenging because only limited testing can be performed in ground facilities. Long duration, full-scale testing requires flight research. Scramjet engines are air-breathing, capturing their oxygen from the atmosphere. Current spacecraft, such as the Space Shuttle, are rocket powered, so they must carry both fuel and oxygen for propulsion. Scramjet technology-based vehicles need to carry only fuel. By eliminating the need to carry oxygen, future hypersonic vehicles will be able to carry heavier payloads. Another unique aspect of the X-43A vehicle is the airframe integration. The body of the vehicle itself forms critical elements of the engine. The forebody acts as part of the intake for airflow and the aft section serves as the nozzle. The X-43A vehicles were manufactured by Micro Craft, Inc., Tullahoma, Tennessee. Orbital Sciences Corporation, Chandler, Arizona, built the Pegasus rocket booster used to launch the X-43 vehicles. For the Dryden research flights, the Pegasus rocket booster and attached X-43 will be air launched by Dryden's B-52 "Mothership." After release from the B-52, the booster will accelerate the X-43A vehicle to the established test conditions (Mach 7 to 10) at an altitude of approximately 100,000 feet where the X-43 will separate from the booster and fly under its own power and preprogrammed control. |
Photo Date |
August 25, 1999 |
|
Hyper-X Research Vehicle - A
Photo Description |
An artist?s conception of the X-43A Hypersonic Experimental Vehicle, or "Hyper-X" in flight. The X-43A was developed to flight test a dual-mode ramjet/scramjet propulsion system at speeds from Mach 7 up to Mach 10 (7 to 10 times the speed of sound, which varies with temperature and altitude). |
Project Description |
Hyper-X, the flight vehicle for which is designated as X-43A, is an experimental flight-research program seeking to demonstrate airframe-integrated, "air-breathing" engine technologies that promise to increase payload capacity for future vehicles, including hypersonic aircraft (faster than Mach 5) and reusable space launchers. This multiyear program is currently underway at NASA Dryden Flight Research Center, Edwards, California. The Hyper-X schedule calls for its first flight later this year (2000). Hyper-X is a joint program, with Dryden sharing responsibility with NASA's Langley Research Center, Hampton, Virginia. Dryden's primary role is to fly three unpiloted X-43A research vehicles to validate engine technologies and hypersonic design tools as well as the hypersonic test facility at Langley. Langley manages the program and leads the technology development effort. The Hyper-X Program seeks to significantly expand the speed boundaries of air-breathing propulsion by being the first aircraft to demonstrate an airframe-integrated, scramjet-powered free flight. Scramjets (supersonic-combustion ramjets) are ramjet engines in which the airflow through the whole engine remains supersonic. Scramjet technology is challenging because only limited testing can be performed in ground facilities. Long duration, full-scale testing requires flight research. Scramjet engines are air-breathing, capturing their oxygen from the atmosphere. Current spacecraft, such as the Space Shuttle, are rocket powered, so they must carry both fuel and oxygen for propulsion. Scramjet technology-based vehicles need to carry only fuel. By eliminating the need to carry oxygen, future hypersonic vehicles will be able to carry heavier payloads. Another unique aspect of the X-43A vehicle is the airframe integration. The body of the vehicle itself forms critical elements of the engine. The forebody acts as part of the intake for airflow and the aft section serves as the nozzle. The X-43A vehicles were manufactured by Micro Craft, Inc., Tullahoma, Tennessee. Orbital Sciences Corporation, Chandler, Arizona, built the Pegasus rocket booster used to launch the X-43 vehicles. For the Dryden research flights, the Pegasus rocket booster and attached X-43 will be air launched by Dryden's B-52 "Mothership." After release from the B-52, the booster will accelerate the X-43A vehicle to the established test conditions (Mach 7 to 10) at an altitude of approximately 100,000 feet where the X-43 will separate from the booster and fly under its own power and preprogrammed control. |
Photo Date |
1997 |
|
Hyper-X Research Vehicle - A
Photo Description |
This is an artist's depiction of a Hyper-X research vehicle under scramjet power in free-flight following separation from its booster rocket. The X-43A was developed to flight test a dual-mode ramjet/scramjet propulsion system at speeds from Mach 7 up to Mach 10 (7 to 10 times the speed of sound, which varies with temperature and altitude). |
Project Description |
Hyper-X, the flight vehicle for which is designated as X-43A, is an experimental flight-research program seeking to demonstrate airframe-integrated, "air-breathing" engine technologies that promise to increase payload capacity for future vehicles, including hypersonic aircraft (faster than Mach 5) and reusable space launchers. This multiyear program is currently underway at NASA Dryden Flight Research Center, Edwards, California. The Hyper-X schedule calls for its first flight later this year (2000). Hyper-X is a joint program, with Dryden sharing responsibility with NASA's Langley Research Center, Hampton, Virginia. Dryden's primary role is to fly three unpiloted X-43A research vehicles to validate engine technologies and hypersonic design tools as well as the hypersonic test facility at Langley. Langley manages the program and leads the technology development effort. The Hyper-X Program seeks to significantly expand the speed boundaries of air-breathing propulsion by being the first aircraft to demonstrate an airframe-integrated, scramjet-powered free flight. Scramjets (supersonic-combustion ramjets) are ramjet engines in which the airflow through the whole engine remains supersonic. Scramjet technology is challenging because only limited testing can be performed in ground facilities. Long duration, full-scale testing requires flight research. Scramjet engines are air-breathing, capturing their oxygen from the atmosphere. Current spacecraft, such as the Space Shuttle, are rocket powered, so they must carry both fuel and oxygen for propulsion. Scramjet technology-based vehicles need to carry only fuel. By eliminating the need to carry oxygen, future hypersonic vehicles will be able to carry heavier payloads. Another unique aspect of the X-43A vehicle is the airframe integration. The body of the vehicle itself forms critical elements of the engine. The forebody acts as part of the intake for airflow and the aft section serves as the nozzle. The X-43A vehicles were manufactured by Micro Craft, Inc., Tullahoma, Tennessee. Orbital Sciences Corporation, Chandler, Arizona, built the Pegasus rocket booster used to launch the X-43 vehicles. For the Dryden research flights, the Pegasus rocket booster and attached X-43 will be air launched by Dryden's B-52 "Mothership." After release from the B-52, the booster will accelerate the X-43A vehicle to the established test conditions (Mach 7 to 10) at an altitude of approximately 100,000 feet where the X-43 will separate from the booster and fly under its own power and preprogrammed control. |
Photo Date |
1997 |
|
Artist Concept of X-43A/Hype
Photo Description |
An artist's conception of the X-43A Hypersonic Experimental Vehicle, or "Hyper-X" in flight. The X-43A was developed to flight test a dual-mode ramjet/scramjet propulsion system at speeds from Mach 7 up to Mach 10 (7 to 10 times the speed of sound, which varies with temperature and altitude). |
Project Description |
Hyper-X, the flight vehicle for which is designated as X-43A, is an experimental flight-research program seeking to demonstrate airframe-integrated, "air-breathing" engine technologies that promise to increase payload capacity for future vehicles, including hypersonic aircraft (faster than Mach 5) and reusable space launchers. This multiyear program is currently underway at NASA Dryden Flight Research Center, Edwards, California. The Hyper-X schedule calls for its first flight later this year (2000). Hyper-X is a joint program, with Dryden sharing responsibility with NASA's Langley Research Center, Hampton, Virginia. Dryden's primary role is to fly three unpiloted X-43A research vehicles to validate engine technologies and hypersonic design tools as well as the hypersonic test facility at Langley. Langley manages the program and leads the technology development effort. The Hyper-X Program seeks to significantly expand the speed boundaries of air-breathing propulsion by being the first aircraft to demonstrate an airframe-integrated, scramjet-powered free flight. Scramjets (supersonic-combustion ramjets) are ramjet engines in which the airflow through the whole engine remains supersonic. Scramjet technology is challenging because only limited testing can be performed in ground facilities. Long duration, full-scale testing requires flight research. Scramjet engines are air-breathing, capturing their oxygen from the atmosphere. Current spacecraft, such as the Space Shuttle, are rocket powered, so they must carry both fuel and oxygen for propulsion. Scramjet technology-based vehicles need to carry only fuel. By eliminating the need to carry oxygen, future hypersonic vehicles will be able to carry heavier payloads. Another unique aspect of the X-43A vehicle is the airframe integration. The body of the vehicle itself forms critical elements of the engine. The forebody acts as part of the intake for airflow and the aft section serves as the nozzle. The X-43A vehicles were manufactured by Micro Craft, Inc., Tullahoma, Tennessee. Orbital Sciences Corporation, Chandler, Arizona, built the Pegasus rocket booster used to launch the X-43 vehicles. For the Dryden research flights, the Pegasus rocket booster and attached X-43 will be air launched by Dryden's B-52 "Mothership." After release from the B-52, the booster will accelerate the X-43A vehicle to the established test conditions (Mach 7 to 10) at an altitude of approximately 100,000 feet where the X-43 will separate from the booster and fly under its own power and preprogrammed control. |
Photo Date |
1998 |
|
X-43A Hypersonic Experimenta
Photo Description |
An artist's conception of the X-43A Hypersonic Experimental Vehicle, or "Hyper-X" in flight. The X-43A was developed to flight test a dual-mode ramjet/scramjet propulsion system at speeds from Mach 7 up to Mach 10 (7 to 10 times the speed of sound, which varies with temperature and altitude). |
Project Description |
Hyper-X, the flight vehicle for which is designated as X-43A, is an experimental flight-research program seeking to demonstrate airframe-integrated, "air-breathing" engine technologies that promise to increase payload capacity for future vehicles, including hypersonic aircraft (faster than Mach 5) and reusable space launchers. This multiyear program is currently underway at NASA Dryden Flight Research Center, Edwards, California. The Hyper-X schedule calls for its first flight later this year (2000). Hyper-X is a joint program, with Dryden sharing responsibility with NASA's Langley Research Center, Hampton, Virginia. Dryden's primary role is to fly three unpiloted X-43A research vehicles to validate engine technologies and hypersonic design tools as well as the hypersonic test facility at Langley. Langley manages the program and leads the technology development effort. The Hyper-X Program seeks to significantly expand the speed boundaries of air-breathing propulsion by being the first aircraft to demonstrate an airframe-integrated, scramjet-powered free flight. Scramjets (supersonic-combustion ramjets) are ramjet engines in which the airflow through the whole engine remains supersonic. Scramjet technology is challenging because only limited testing can be performed in ground facilities. Long duration, full-scale testing requires flight research. Scramjet engines are air-breathing, capturing their oxygen from the atmosphere. Current spacecraft, such as the Space Shuttle, are rocket powered, so they must carry both fuel and oxygen for propulsion. Scramjet technology-based vehicles need to carry only fuel. By eliminating the need to carry oxygen, future hypersonic vehicles will be able to carry heavier payloads. Another unique aspect of the X-43A vehicle is the airframe integration. The body of the vehicle itself forms critical elements of the engine. The forebody acts as part of the intake for airflow and the aft section serves as the nozzle. The X-43A vehicles were manufactured by Micro Craft, Inc., Tullahoma, Tennessee. Orbital Sciences Corporation, Chandler, Arizona, built the Pegasus rocket booster used to launch the X-43 vehicles. For the Dryden research flights, the Pegasus rocket booster and attached X-43 will be air launched by Dryden's B-52 "Mothership." After release from the B-52, the booster will accelerate the X-43A vehicle to the established test conditions (Mach 7 to 10) at an altitude of approximately 100,000 feet where the X-43 will separate from the booster and fly under its own power and preprogrammed control. |
Photo Date |
1999 |
|
Photo Description |
Mach 7 wind tunnel test of the full-scale X-43A model with spare flight engine in Langley's 8-Foot High Temperature Tunnel. |
Project Description |
The experimental X-43A hypersonic research aircraft, part aircraft and part spacecraft, will be dropped from the wing of a modified B-52 aircraft, boosted to nearly 100,000 feet altitude by a booster rocket and released over the Pacific Ocean to briefly fly under its own power at seven times the speed of sound, almost 5,000 mph. The flight is part of the Hyper-X program, a research effort designed to demonstrate alternate propulsion technologies for access to space and high-speed flight within the atmosphere. It will provide unique "first time" free flight data on hypersonic air-breathing engine technologies that have large potential pay-offs. The $250 million program began with conceptual design and scramjet engine wind tunnel work in 1996. In a scramjet (supersonic-combustion ramjet), the flow of air through the engine remains supersonic, or greater than the speed of sound, for optimum engine efficiency and vehicle speed. A scramjet operates by supersonic combustion of fuel in a stream of air com,pressed by the high forward speed of the aircraft, as opposed to a normal jet engine, in which the compressor blades compress the air. Scramjets start operation at about Mach 6, or six times the speed of sound. There are few or no moving parts in a scramjet engine, but achieving proper ignition and combustion in a matter of milliseconds proved to be an engineering challenge of the highest order. Researchers believe these technologies may someday offer more airplane-like operations and other benefits compared to traditional rocket systems. Rockets provide limited throttle control and must carry heavy tanks filled with liquid oxygen, necessary for combustion of fuel. An air-breathing engine, like that on the X-43A, scoops oxygen from the air as it flies. The weight savings could be used to increase payload capacity, increase range or reduce vehicle size for the same payload. NASA's Langley Research Center, Hampton, Va., and Dryden Flight Research Center, Edwards, Calif., jointly conduct the Hyper-X program. ATK-GASL (formerly Microcraft, Inc.) of Tullahoma, Tenn., built both the X-43A aircraft and the scramjet engine, and Boeing Phantom Works, Huntington Beach, Calif., designed the thermal protection and onboard systems. The booster is a modified first stage of a Pegasus rocket built by Orbital Sciences Corp, Chandler, Ariz. |
Photo Date |
unknown |
|
Lockheed Electra - animation
SOFIA
NASA's SOFIA infrared observ
8/27/09
Description |
NASA's SOFIA infrared observatory 747SP overflies its home, the Dryden Aircraft Operations Facility in Palmdale, Calif. January 15, 2008 NASA Photo / Jim Ross ED08-0015-28 |
Date |
8/27/09 |
|
A Crane Lifts SOFIA's Newly
A crane is used to lift SOFI
10/28/08
Description |
A crane is used to lift SOFIA's newly coated primary mirror assembly from the floor of NASA's Dryden Aircraft Operations Facility, Palmdale, Calif. October 8, 2008 NASA Photo / Carla Thomas ED08-0262-35 › Read News Release 08-50 |
Date |
10/28/08 |
|
SOFIA
ED09-0089-86 Several NASA sc
4/10/09
Description |
ED09-0089-86 Several NASA science aircraft, including (from bottom) the SOFIA observatory, the DC-8 airborne laboratory and an ER-2 high-altitude aircraft, along with one of NASA's modified 747 Shuttle Carrier Aircraft, occupied the Dryden Aircraft Operations Facility during dedication ceremonies and an open house for employees and their families on April 9, 2009. (NASA photo / Tom Tschida) April 9, 2009 NASA photo / Tom Tschida |
Date |
4/10/09 |
|
SOFIA
ED09-0089-90 Several NASA ai
4/10/09
Description |
ED09-0089-90 Several NASA aircraft, including the SOFIA observatory in the foreground, the DC-8 airborne laboratory, an ER-2 high-altitude science aircraft and one of NASA's modified 747 Shuttle Carrier Aircraft at upper left and a Gulfstream III and a B-200 King Air at far right, occupied the Dryden Aircraft Operations Facility during dedication ceremonies on April 9, 2009 NASA photo / Tom Tschida |
Date |
4/10/09 |
|
SOFIA
ED09-0279-27 The Stratospher
10/6/09
Description |
ED09-0279-27 The Stratospheric Observatory for Infrared Astronomy science team completed checkout of optical star tracking camera systems and conducted telescope assembly preparation exercises during nighttime testing on the ramp at the Dryden Aircraft Operations Facility in Palmdale, Calif. September 24, 2009 NASA Photo / Tom Tschida |
Date |
10/6/09 |
|
SOFIA
ED09-0279-35 The Stratospher
10/6/09
Description |
ED09-0279-35 The Stratospheric Observatory for Infrared Astronomy's 747SP sits on an aircraft ramp during nighttime testing and operation of the SOFIA's German-built telescope assembly. The aircraft is based at NASA's Dryden Aircraft Operations Facility in Palmdale, Calif. September 24, 2009 NASA Photo / Tom Tschida |
Date |
10/6/09 |
|
SOFIA
ED09-0279-38 The Stratospher
10/6/09
Description |
ED09-0279-38 The Stratospheric Observatory for Infrared Astronomy's 747SP is illuminated prior to nighttime testing and operation of the German-built telescope assembly. The aircraft is based at NASA's Dryden Operations Facility in Palmdale, Calif. September 24, 2009 NASA Photo / Tom Tschida |
Date |
10/6/09 |
|
SOFIA
ED10-0115-18 In this long-ex
05/20/10
Description |
ED10-0115-18 In this long-exposure image, the 2.5-meter infrared telescope peers out at a starry sky from its cavity in the rear fuselage of NASA's highly modified Stratospheric Observatory for Infrared Astronomy Boeing 747SP during nighttime line operations testing. The line operations tests at the Dryden Aircraft Operations Facility in Palmdale, Calif., enable the SOFIA aircraft, telescope, and FORCAST teams to prepare for the flying observatory's upcoming 'first light' science flights. May 20, 2010 NASA/Tom Tschida |
Date |
05/20/10 |
|
SOFIA
ED10-0115-21 A sharp eye can
05/20/10
Description |
ED10-0115-21 A sharp eye can pick out faint specks of stars reflected by the 100-inch 2.5 meter primary mirror on NASA's Stratospheric Observatory for Infrared Astronomy SOFIA during ground testing of the Faint Object Infrared Camera for the SOFIA Telescope FORCAST. The line operations tests at the Dryden Aircraft Operations Facility in Palmdale, Calif., enabled the SOFIA aircraft, telescope, and FORCAST teams to prepare for the flying observatory's 'first light' astronomical science flights. May 20, 2010 NASA/Tom Tschida |
Date |
05/20/10 |
|
SOFIA
ED10-0115-23 Faint specks of
05/20/10
Description |
ED10-0115-23 Faint specks of starlight are reflected by the 100-inch 2.5 meter primary mirror on NASA's Stratospheric Observatory for Infrared Astronomy SOFIA during ground testing of the Faint Object Infrared Camera for the SOFIA Telescope FORCAST. The line operations tests at the Dryden Aircraft Operations Facility in Palmdale, Calif., enabled the SOFIA aircraft, telescope, and FORCAST teams to prepare for the flying observatory's upcoming 'first light' science flights. May 20, 2010 NASA/Tom Tschida |
Date |
05/20/10 |
|
Dave Kratz
Dave Kratz with the Climate
5/13/08
Description |
Dave Kratz with the Climate Science Branch sets up the solar telescope on the great lawn in front of the Ferguson Center for the Arts for participants attending EarthFest. The connection between the sun and the Earth is important for researchers at NASA Langley as they study climate change and the balance of energy and heat in our atmosphere. Credit: NASA/Sean Smith |
Date |
5/13/08 |
|
Discovery Kiosk
Guests at EarthFest were abl
5/13/08
Description |
Guests at EarthFest were able to learn about NASA Langley's scientific research through many activities. Here, Nancy Holloway from the Fabrication Technology Development Branch and her daughter, Hannah, discover scientific benefits to society, like advances in aviation safety and coastal management. Credit: NASA/Sean Smith |
Date |
5/13/08 |
|
Ares Lift
Hardware is being fabricated
12/1/08
Description |
Hardware is being fabricated at NASA Langley prior to airlifting to NASA's Kennedy Space Center for flight test next year. Pictured is a major element of the Ares I-X Crew Module/Launch Abort System simulator. The elements will simulate the topmost parts of the Ares I-X, the rocket designed to demonstrate technologies for NASA's next generation of crewed spacecraft. Credit: NASA/Sean Smith |
Date |
12/1/08 |
|
Pathfinder Crew Module With
Langley engineers and techni
3/2/09
Description |
Langley engineers and technicians recently mated together the Pathfinder Crew Module with the PA-1 Separation Ring. This hardware will be used at White Sands Missile Range in New Mexico to help prepare for the first test of the launch abort system, called Pad Abort 1. Credit: NASA/Sean Smith |
Date |
3/2/09 |
|
The Road to Apollo
Project Fire explored the in
3/9/09
Description |
Project Fire explored the intense heat of atmospheric reentry and its effects on would-be spacecraft materials. Although the ultimate tests involved Atlas rockets carrying recoverable reentry packages, the flight tests from Cape Canaveral were preceded by a series of important wind-tunnel tests at Langley. Here technicians ready materials for a high-temperature wind tunnel test. Credit: NASA |
Date |
3/9/09 |
|
Orion Launch Abort System Pa
The launch abort system path
3/10/09
Description |
The launch abort system pathfinder hit the road on Tuesday from NASA Langley in Hampton, Va., and is on its way to White Sands Missile Range in New Mexico. The pathfinder will support the first flight test of the abort system, called Pad Abort 1. Credit: NASA/Sean Smith &rsaquo, Learn More |
Date |
3/10/09 |
|
Yuri's Night Hampton Roads
Vincent Whitfield, public ou
3/30/09
Description |
Vincent Whitfield, public outreach specialist at NASA Langley, visited Christopher Newport University on Tuesday dressed as an astronaut to excite students about Yuri's Night Hampton Roads, a celebration of space exploration that will take place Saturday, April 4, from 7 p.m. to midnight at the Virginia Air & Space Center. Pictured from left to right: Shaun Johnson, Vincent Whitfield, Mike W., and Patrick Burke. Credit: NASA/Sean Smith |
Date |
3/30/09 |
|
The Road to Apollo 07: John
In the opinion of many space
4/6/09
Description |
In the opinion of many space historians, Langley's most important contribution to the Apollo program was its development of Lunar Orbit Rendezvous (LOR). Here, John Houbolt explains the critical weight-saving advantage of the LOR concept. The basic premise was to fire an assembly of three spacecraft into Earth orbit on top of a single powerful rocket. Without this successful mission concept, the United States may still have landed humans on the moon, but it probably would not have happened by the end of the 1960s as directed by President Kennedy. Credit: NASA |
Date |
4/6/09 |
|
The Road to Apollo
After Mercury came Gemini, t
4/6/09
Description |
After Mercury came Gemini, the project that would put to the test the maneuvers that would be required if Apollo was to be successful. Gemini astronauts would have to practice the rendezvous and docking techniques necessary to link two spacecraft. Langley researchers built the Rendezvous Docking Simulator giving astronauts a routine opportunity to pilot dynamically-controlled scale-model vehicles in an environment that closely paralleled that of space. Credit: NASA |
Date |
4/6/09 |
|
The Road to Apollo
The most successful of the p
4/21/09
Description |
The most successful of the pre-Apollo probes, Lunar Orbiter photographically mapped the equatorial regions of the moon. These maps, compiled at Langley, provided the detailed topographical information needed to pinpoint the best landing sites on the moon, including the exact spot in the Sea of Tranquility chosen for Apollo 11. Credit: NASA |
Date |
4/21/09 |
|
United We Serve -- Karen Ste
Karen Steele and her husband
8/11/09
Description |
Karen Steele and her husband, Bill Pardue, prefer to be "doers" and not just "sayers." They have made themselves living examples for years by helping just about anywhere their help was needed. They wanted to aid worthy causes, and if they couldn't help financially they just donated their time and effort. Steele works at NASA Langley with the contracts group for ROME. Her husband is a Chrysler technician in Smithfield. They live in Gates County, N.C. Many of their nights and weekends are devoted to jobs that pay solely in gratitude. |
Date |
8/11/09 |
|
NACA Dryden test pilot Howar
Dryden and Victory welcomed
Title |
Dryden and Victory welcomed by Reid |
Description |
Hugh L. Dryden (left), George Lewis's successor as the NACA's director of research, arrives with John F. Victory, the NACA's executive secretary, for a tour of the Langley Memorial Aeronautical Laboratory (LMAL). Welcoming Dryden and Victory is engineer-in-charge Henry Reid. Photograph published in Engineer in Charge: A History of the Langley Aeronautical Laboratory, 1917-1958 by James R. Hansen (page 217). |
Date |
09.11.1947 |
|
HL-10 on ramp
Photo Description |
The HL-10, seen here parked on the ramp, was one of five lifting body designs flown at NASA's Dryden Flight Research Center, Edwards, California, from July 1966 to November 1975 to study and validate the concept of safely maneuvering and landing a low lift-over-drag vehicle designed for reentry from space. |
Project Description |
Northrop Corporation built the HL-10 and M2-F2, the first two of the fleet of "heavy" lifting bodies flown by the NASA Flight Research Center. The contract for construction of the HL-10 and the M2-F2 was $1.8 million. "HL" stands for horizontal landing, and "10" refers to the tenth design studied by engineers at NASA's Langley Research Center, Hampton, Va. After delivery to NASA in January 1966, the HL-10 made its first flight on Dec. 22, 1966, with research pilot Bruce Peterson in the cockpit. Although an XLR-11 rocket engine was installed in the vehicle, the first 11 drop flights from the B-52 launch aircraft were powerless glide flights to assess handling qualities, stability, and control. In the end, the HL-10 was judged to be the best handling of the three original heavy-weight lifting bodies (M2-F2/F3, HL-10, X-24A). The HL-10 was flown 37 times during the lifting body research program and logged the highest altitude and fastest speed in the Lifting Body program. On Feb. 18, 1970, Air Force test pilot Peter Hoag piloted the HL-10 to Mach 1.86 (1,228 mph). Nine days later, NASA pilot Bill Dana flew the vehicle to 90,030 feet, which became the highest altitude reached in the program. Some new and different lessons were learned through the successful flight testing of the HL-10. These lessons, when combined with information from it's sister ship, the M2-F2/F3, provided an excellent starting point for designers of future entry vehicles, including the Space Shuttle. |
Photo Date |
May 27, 1966 |
|
Dryden research pilot Gordon
Long-time NASA Dryden resear
8/29/08
Description |
Long-time NASA Dryden research pilot and former astronaut C. Gordon Fullerton capped an almost 50-year flying career, including more than 38 years with NASA, with a final flight in a NASA F/A-18 on Dec. 21, 2007. Fullerton and Dryden research pilot Jim Smolka flew a 90-minute pilot proficiency formation aerobatics flight with another Dryden F/A-18 and a Dryden T-38 before concluding with two low-level formation flyovers of Dryden before landing. Fullerton was honored with a water-cannon spray arch provided by two fire trucks from the Edwards Air Force Base fire department as he taxied the F/A-18 up to the Dryden ramp, and was then greeted by his wife Marie and several hundred Dryden staff after his final flight. December 21, 2007 NASA / Photo Tony Landis ED07-0294-27 |
Date |
8/29/08 |
|
M2-F1 in flight on tow line
Photo Description |
The M2-F1 Lifting Body is seen here under tow at the Flight Research Center (later redesignated the Dryden Flight Research Center), Edwards, California. |
Project Description |
The wingless, lifting-body aircraft design was initially conceived as a means of landing an aircraft horizontally after atmospheric reentry. The absence of wings would make the extreme heat of re-entry less damaging to the vehicle. In 1962, Flight Research Center management approved a program to build a lightweight, unpowered lifting body as a prototype to flight test the wingless concept. It would look like a "flying bathtub," and was designated the M2-F1, the "M" referring to "manned" and "F" referring to "flight" version. It featured a plywood shell placed over a tubular steel frame crafted at Dryden. Construction was completed in 1963. The M2-F1 project had limited goals. They were to show that a piloted lifting body could be built, that it could not only fly but be controlled in flight, and that it could make a successful landing. While the M2-F1 did prove the concept, with a wooden fuselage and fixed landing gear, it was far from an operational spacecraft. The next step in the lifting-body development was to build a heavyweight, rocket-powered vehicle that was more like an operational lifting body, albeit one without the thermal protection system that would be needed for reentry into the atmosphere from space at near-orbital speeds. The first flight tests of the M2-F1 were over Rogers Dry Lake at the end of a tow rope attached to a hopped-up Pontiac convertible driven at speeds up to about 120 mph. These initial tests produced enough flight data about the M2-F1 to proceed with flights behind a NASA C-47 tow plane at greater altitudes. The C-47 took the craft to an altitude of 12,000 where free flights back to Rogers Dry Lake began. Pilot for the first series of flights of the M2-F1 was NASA research pilot Milt Thompson. Typical glide flights with the M2-F1 lasted about two minutes and reached speeds of 110 to 120 mph. More than 400 ground tows and 77 aircraft tow flights were carried out with the M2-F1. The success of Dryden's M2-F1 program led to NASA's development and construction of two heavyweight lifting bodies based on studies at NASA's Ames and Langley research centers--the M2-F2 and the HL-10, both built by the Northrop Corporation, and the U.S. Air Force's X-24 program. The Lifting Body program also heavily influenced the Space Shuttle program. The M2-F1 program demonstrated the feasibility of the lifting body concept for horizontal landings of atmospheric entry vehicles. It also demonstrated a procurement and management concept for prototype flight test vehicles that produced rapid results at very low cost (approximately $50,000, excluding salaries of government employees assigned to the project). |
Photo Date |
August 28, 1964 |
|
Active Sensing of CO2 Emissi
Researchers from the Science
11/24/08
Description |
Researchers from the Science Directorate at NASA Langley are working to better understand Earth's atmosphere and our changing climate. One group within the SD has partnered with ITT in Fort Wayne, Ind., to build and test a laser instrument called ASCENDS -- short for Active Sensing of CO<sub>2</sub> Emissions over Nights, Days, and Seasons -- to study atmospheric carbon dioxide, an important greenhouse gas that is know to influence climate change. This fall, the teams met at the LaRC hangar to test-fly the instrument's Engineering Development Unit on the LaRC UC-12, a new aircraft at NASA Langley. In this photo, Mike Dobbs, instrument Co-Principal Investigator from ITT, pours liquid nitrogen to be used to cool the laser detector while in flight. The UC-12 is directly behind Dobbs awaiting take-off. Ultimately, the ASCENDS team hopes to see their instrument concept flown in space as Advanced CO<sub>2</sub> and Climate Laser International Mission (ACCLAIM), one of the 15 missions of critical importance recommended by the 2007 decadal survey for Earth science. Credit: NASA/Sean Smith |
Date |
11/24/08 |
|
Smile, It's A Beautiful Day!
Mysterious chalkings have be
4/28/09
Description |
Mysterious chalkings have been reported throughout NASA Langley Research Center. The puzzling messages appeared overnight and urge employees to take bizarre actions, such as smile, dance through crosswalks and skip to work. Safety officials tested the chalk and have confirmed that it presents no problem to employees. Langley spokesperson Marny Skora says management encourages employees to take risks, noting that as one chalking indicates, "Every noble work is at first impossible." Credit: NASA/Sean Smith |
Date |
4/28/09 |
|
Every Noble Work...
Mysterious chalkings have be
4/28/09
Description |
Mysterious chalkings have been reported throughout NASA Langley Research Center. The puzzling messages appeared overnight and urge employees to take bizarre actions, such as smile, dance through crosswalks and skip to work. Safety officials tested the chalk and have confirmed that it presents no problem to employees. Langley spokesperson Marny Skora says management encourages employees to take risks, noting that as one chalking indicates, "Every noble work is at first impossible." Credit: NASA/Sean Smith |
Date |
4/28/09 |
|
Smile!
Mysterious chalkings have be
4/28/09
Description |
Mysterious chalkings have been reported throughout NASA Langley Research Center. The puzzling messages appeared overnight and urge employees to take bizarre actions, such as smile, dance through crosswalks and skip to work. Safety officials tested the chalk and have confirmed that it presents no problem to employees. Langley spokesperson Marny Skora says management encourages employees to take risks, noting that as one chalking indicates, "Every noble work is at first impossible." Credit: NASA/Sean Smith |
Date |
4/28/09 |
|
NACA Groundbreaking Ceremony
Photo Date |
January 27, 1953 |
|
Unveiling of sign for Walter
Lobby View
From above, EarthFest activi
5/13/08
Description |
From above, EarthFest activities are spread out in one of the lobbies of the Ferguson Center for the Arts. Some of the activities on display in this space are the student art competition, CNU student clubs and activities, face-painting and a group mural sponsored by the Peninsula Fine Art Center, and a musical performance by the Prisoners. Credit: NASA/Sean Smith |
Date |
5/13/08 |
|
Devin Smith
The "carbon footprint" theme
5/13/08
Description |
The "carbon footprint" theme was used throughout EarthFest, with footprints leading the way from one activity to the next. Here, Devin Smith measures his feet against one of the carbon footprints. Credit: NASA/Sean Smith |
Date |
5/13/08 |
|
Astronaut Mary Cleave
Former NASA Astronaut Mary C
5/13/08
Description |
Former NASA Astronaut Mary Cleave gives the keynote address at EarthFest, addressing the guests on the importance of studying our home planet. Credit: NASA/Sean Smith |
Date |
5/13/08 |
|
EarthFest Chess
The Christopher Newport Univ
5/13/08
Description |
The Christopher Newport University Chess Club set up a large chess set outside of the Ferguson Center for the Arts. On the left is David Carter, a junior theater major at CNU, going head-to-head against Jack Nichting, a seventh grader. Nichting won the match. Credit: NASA/Sean Smith |
Date |
5/13/08 |
|
EarthFest Face Painting
Juliann and Colleen Rink, da
5/13/08
Description |
Juliann and Colleen Rink, daughters of Chris Rink of the Office of Strategic Communications and Education, got their faces painted and took part in the group Earth mural at EarthFest. Credit: NASA/Sean Smith |
Date |
5/13/08 |
|
EarthFest 2008: CNU Chemistr
Christopher Newport Universi
5/13/08
Description |
Christopher Newport University students, Christine Allen, left, and Sheena Clift, right, staff a dispCNlay for the CNU Chemistry Club at EarthFest. The students show off lab-produced bio-diesel fuel as well as information on "green" cleaning products. Credit: NASA/Sean Smith |
Date |
5/13/08 |
|
The Road to Apollo
The challenge: fly humans a
2/23/09
Description |
The challenge: fly humans a quarter of a million miles, make a pinpoint landing on a strange planet, blast off and return home safely after an eight-day voyage through space. This photograph of Lunar Excursion Module pilot Buzz Aldrin on the lunar surface was taken by Apollo 11 commander Neil Armstrong. Credit: NASA |
Date |
2/23/09 |
|
Inspecting the 14 x 22 Wind
Frank Quinto, facility manag
2/13/09
Description |
Frank Quinto, facility manager for the 14- by 22 Foot Subsonic Tunnel, inspects the fan blade area of the tunnel. Technicians erected scaffolding (in the background) to remove the blades for minor repairs. The fan blades will be re-installed so the tunnel can be up and running again by the end of the month. Credit: NASA/Sean Smith |
Date |
2/13/09 |
|
The Road to Apollo
The Scout program began in 1
3/2/09
Description |
The Scout program began in 1957 to build an inexpensive sounding rocket to carry small research payloads to high altitudes. Scout would eventually assist the Mercury, Gemini and Apollo programs by testing reentry materials, evaluating methods of protecting spacecraft from micrometeoroids, and examining ways of overcoming radio blackouts as a space capsule reentered the atmosphere. The first Scout launched at Wallops Island July 1, 1960. Credit: NASA |
Date |
3/2/09 |
|
Ares I Testing
Wind tunnel manager Frank Qu
9/18/09
Description |
Wind tunnel manager Frank Quinto explains how a model of the NASA Ares I rocket will be tested in the 14 x 22 Foot Subsonic Tunnel. The test series will help confirm that the Ares I can safely withstand winds while sitting on the launch pad. Credit: NASA/Sean Smith |
Date |
9/18/09 |
|
Virtusphere
Jim Dimascio demonstrates th
10/2/09
Description |
Jim Dimascio demonstrates the Virtusphere inside the Reid Center as Ray Latypov looks on. The Virtusphere is a locomotion platform that allows users to be completely immersed into their interactive virtual experience. Latypov and Dimascio, owners of Virtusphere, Inc. based in New York, brought the 10-foot (3 m) high structure to Langley Oct. 1 for a demonstration in the Reid Center. Jeff Antol with the Space Mission Anaylsis Branch arranged the visit to show employees how NASA Langley is pushing the envelope and studying immersive applications for exploration. Besides gaming and military training, the Virtusphere could be used by scientists and researchers to create an environment using real data that simlulates exploring on the Lunar or Mars surface. Credit: NASA/Sean Smith |
Date |
10/2/09 |
|
Crew Impact Attenuation Syst
Steve Nevins examines instru
2/20/09
Description |
Steve Nevins examines instrumentation next to the Crew Impact Attenuation System (CIAS) Test Article in the garage across from building 1297. Langley engineers recently designed and fabricated the 20,000-pound test article which completed seven preliminary impact tests at Langley's Landing and Impact Dynamics gantry since the start of the year. Later this month, technicians will attach energy absorbing struts to ready the hardware for testing the Orion seat pallet system. The CIAS test article emulates the Orion crew module interface to the seat pallet that will accommodate between four and six astronauts. Once energy absorbing struts are attached to the seat pallet, a new phase of testing for Orion will begin. The series of tests will evaluate Orion's energy absorbing seat system, which will help reduce loads on the astronauts and protect them from injury when returning to Earth from a mission to the International Space Station or the moon. Credit: NASA/Sean Smith |
Date |
2/20/09 |
|
Photo Description |
The second X-43A hypersonic research aircraft, attached to a modified Pegasus booster rocket and followed by a chase F-18, was taken to launch altitude by NASA's B-52B launch aircraft from the NASA Dryden Flight Research Center at Edwards Air Force Base, Calif., on March 27, 2004. About an hour later the Pegasus booster was released from the B-52 to accelerate the X-43A to its intended speed of Mach 7. In a combined research effort involving Dryden, Langley, and several industry partners, NASA demonstrated the value of its X-43A hypersonic research aircraft, as it became the first air-breathing, unpiloted, scramjet-powered plane to fly freely by itself. The March 27 flight, originating from NASA's Dryden Flight Research Center, began with the Agency's B-52B launch aircraft carrying the X-43A out to the test range over the Pacific Ocean off the California coast. The X-43A was boosted up to its test altitude of about 95,000 feet, where it separated from its modified Pegasus booster and flew freely under its own power. Two very significant aviation milestones occurred during this test flight: first, controlled accelerating flight at Mach 7 under scramjet power, and second, the successful stage separation at high dynamic pressure of two non-axisymmetric vehicles. To top it all off, the flight resulted in the setting of a new aeronautical speed record. The X-43A reached a speed of over Mach 7, or about 5,000 miles per hour faster than any known aircraft powered by an air-breathing engine has ever flown. |
Project Description |
The high-risk, high-payoff X-43A flights are the first actual flight tests of an aircraft powered by a scramjet engine capable of operating at hypersonic speeds (above Mach 5, or five times the speed of sound). The X-43A is powered by a revolutionary air-breathing supersonic-combustion ramjet or "scramjet" engine. |
Photo Date |
March 27, 2004 |
|
Photo Description |
The second X-43A hypersonic research aircraft and its modified Pegasus booster rocket accelerate after launch from NASA's B-52B launch aircraft over the Pacific Ocean on March 27, 2004. The mission originated from the NASA Dryden Flight Research Center at Edwards Air Force Base, Calif. Minutes later the X-43A separated from the Pegasus booster and accelerated to its intended speed of Mach 7. In a combined research effort involving Dryden, Langley, and several industry partners, NASA demonstrated the value of its X-43A hypersonic research aircraft, as it became the first air-breathing, unpiloted, scramjet-powered plane to fly freely by itself. The March 27 flight, originating from NASA's Dryden Flight Research Center, began with the Agency's B-52B launch aircraft carrying the X-43A out to the test range over the Pacific Ocean off the California coast. The X-43A was boosted up to its test altitude of about 95,000 feet, where it separated from its modified Pegasus booster and flew freely under its own power. Two very significant aviation milestones occurred during this test flight: first, controlled accelerating flight at Mach 7 under scramjet power, and second, the successful stage separation at high dynamic pressure of two non-axisymmetric vehicles. To top it all off, the flight resulted in the setting of a new aeronautical speed record. The X-43A reached a speed of over Mach 7, or about 5,000 miles per hour faster than any known aircraft powered by an air-breathing engine has ever flown. |
Project Description |
The high-risk, high-payoff X-43A flights are the first actual flight tests of an aircraft powered by a scramjet engine capable of operating at hypersonic speeds (above Mach 5, or five times the speed of sound). The X-43A is powered by a revolutionary air-breathing supersonic-combustion ramjet or "scramjet" engine. |
Photo Date |
March 27, 2004 |
|
NASA Dryden Salutes Our Nati
ED08-0304-45 On the 233rd an
7/2/09
Description |
ED08-0304-45 On the 233rd anniversary of the United States of America's Declaration of Independence, NASA's Dryden Flight Research Center salutes our nation's flag on Independence Day weekend 2009. NASA Dryden photographer Tom Tschida created this composite image from an original image taken by Dryden photographer Carla Thomas of NASA Dryden's four F/A-18 mission support aircraft during a formation pilot proficiency flight on . Nov. 24, 2008 NASA Photo Carla Thomas / Tom Tschida |
Date |
7/2/09 |
|
NASA Connect - Crash - ALDF
NASA Connect segment explain
10/1/00
Description |
NASA Connect segment explaining NASA Langley's Aircraft Landing Dynamics Facility, or ALDF. The video explores how scientists are using math and technology to test tires, wheels, and brakes. |
Date |
10/1/00 |
|
Photo Description |
The second X-43A hypersonic research aircraft and its modified Pegasus booster rocket drop away from NASA's B-52B launch aircraft over the Pacific Ocean on March 27, 2004. The mission originated from the NASA Dryden Flight Research Center at Edwards Air Force Base, Calif. Moments later the Pegasus booster ignited to accelerate the X-43A to its intended speed of Mach 7. |
Project Description |
The high-risk, unpiloted X-43A flights are the first actual flight tests of an aircraft powered by a scramjet engine capable of operating at hypersonic speeds (above Mach 5, or five times the speed of sound). The X-43A is powered by a revolutionary air-breathing supersonic-combustion ramjet or "scramjet" engine. In a combined research effort involving Dryden, Langley, and several industry partners, NASA demonstrated the value of its X-43A hypersonic research aircraft, as it became the first air-breathing, unpiloted, scramjet-powered plane to fly freely by itself. The March 27 flight, originating from NASA's Dryden Flight Research Center, began with the Agency's B-52B launch aircraft carrying the X-43A out to the test range over the Pacific Ocean off the California coast. The X-43A was boosted up to its test altitude of about 95,000 feet, where it separated from its modified Pegasus booster and flew freely under its own power. Two very significant aviation milestones occurred during this test flight: first, controlled accelerating flight at Mach 7 under scramjet power, and second, the successful stage separation at high dynamic pressure of two non-axisymmetric vehicles. To top it all off, the flight resulted in the setting of a new aeronautical speed record. The X-43A reached a speed of over Mach 7, or about 5,000 miles per hour faster than any known aircraft powered by an air-breathing engine has ever flown. |
Photo Date |
March 27, 2004 |
|
Photo Description |
The second X-43A hypersonic research aircraft and its modified Pegasus booster rocket accelerate after launch from NASA's B-52B launch aircraft over the Pacific Ocean on March 27, 2004. The mission originated from the NASA Dryden Flight Research Center at Edwards Air Force Base, Calif. Minutes later the X-43A separated from the Pegasus booster and accelerated to its intended speed of Mach 7. |
Project Description |
The high-risk, high-payoff X-43A flights are the first actual flight tests of an aircraft powered by a scramjet engine capable of operating at hypersonic speeds (above Mach 5, or five times the speed of sound). The X-43A is powered by a revolutionary air-breathing supersonic-combustion ramjet or "scramjet" engine. In a combined research effort involving Dryden, Langley, and several industry partners, NASA demonstrated the value of its X-43A hypersonic research aircraft, as it became the first air-breathing, unpiloted, scramjet-powered plane to fly freely by itself. The March 27 flight, originating from NASA's Dryden Flight Research Center, began with the Agency's B-52B launch aircraft carrying the X-43A out to the test range over the Pacific Ocean off the California coast. The X-43A was boosted up to its test altitude of about 95,000 feet, where it separated from its modified Pegasus booster and flew freely under its own power. Two very significant aviation milestones occurred during this test flight: first, controlled accelerating flight at Mach 7 under scramjet power, and second, the successful stage separation at high dynamic pressure of two non-axisymmetric vehicles. To top it all off, the flight resulted in the setting of a new aeronautical speed record. The X-43A reached a speed of over Mach 7, or about 5,000 miles per hour faster than any known aircraft powered by an air-breathing engine has ever flown. |
Photo Date |
March 27, 2004 |
|
Photo Description |
The second X-43A hypersonic research aircraft and its modified Pegasus booster rocket left the runway, carried aloft by NASA's B-52B launch aircraft from the NASA Dryden Flight Research Center at Edwards Air Force Base, Calif., on March 27, 2004. About an hour later the Pegasus booster was launched from the B-52 to accelerate the X-43A to its intended speed of Mach 7. |
Project Description |
The high-risk, high-payoff X-43A flights are the first actual flight tests of an aircraft powered by a scramjet engine capable of operating at hypersonic speeds (above Mach 5, or five times the speed of sound). The X-43A is powered by a revolutionary air-breathing supersonic-combustion ramjet or "scramjet" engine. In a combined research effort involving Dryden, Langley, and several industry partners, NASA demonstrated the value of its X-43A hypersonic research aircraft, as it became the first air-breathing, unpiloted, scramjet-powered plane to fly freely by itself. The March 27 flight, originating from NASA's Dryden Flight Research Center, began with the Agency's B-52B launch aircraft carrying the X-43A out to the test range over the Pacific Ocean off the California coast. The X-43A was boosted up to its test altitude of about 95,000 feet, where it separated from its modified Pegasus booster and flew freely under its own power. Two very significant aviation milestones occurred during this test flight: first, controlled accelerating flight at Mach 7 under scramjet power, and second, the successful stage separation at high dynamic pressure of two non-axisymmetric vehicles. To top it all off, the flight resulted in the setting of a new aeronautical speed record. The X-43A reached a speed of over Mach 7, or about 5,000 miles per hour faster than any known aircraft powered by an air-breathing engine has ever flown. |
Photo Date |
March 27, 2004 |
|
Photo Description |
NASA's B-52B aircraft over the Dryden Flight Research Center after the successful launch of the second X-43A hypersonic research vehicle. |
Project Description |
The high-risk, high-payoff X-43A flights are the first actual flight tests of an aircraft powered by a scramjet engine capable of operating at hypersonic speeds (above Mach 5, or five times the speed of sound). The X-43A is powered by a revolutionary air-breathing supersonic-combustion ramjet or "scramjet" engine. In a combined research effort involving Dryden, Langley, and several industry partners, NASA demonstrated the value of its X-43A hypersonic research aircraft, as it became the first air-breathing, unpiloted, scramjet-powered plane to fly freely by itself. The March 27 flight, originating from NASA's Dryden Flight Research Center, began with the Agency's B-52B launch aircraft carrying the X-43A out to the test range over the Pacific Ocean off the California coast. The X-43A was boosted up to its test altitude of about 95,000 feet, where it separated from its modified Pegasus booster and flew freely under its own power. Two very significant aviation milestones occurred during this test flight: first, controlled accelerating flight at Mach 7 under scramjet power, and second, the successful stage separation at high dynamic pressure of two non-axisymmetric vehicles. To top it all off, the flight resulted in the setting of a new aeronautical speed record. The X-43A reached a speed of over Mach 7, or about 5,000 miles per hour faster than any known aircraft powered by an air-breathing engine has ever flown. |
Photo Date |
March 27, 2004 |
|
Photo Description |
The second X-43A hypersonic research aircraft and its modified Pegasus booster rocket left the runway, carried aloft by NASA's B-52B launch aircraft from the NASA Dryden Flight Research Center at Edwards Air Force Base, Calif., on March 27, 2004. About an hour later the Pegasus booster was launched from the B-52 to accelerate the X-43A to its intended speed of Mach 7. |
Project Description |
The high-risk, high-payoff X-43A flights are the first actual flight tests of an aircraft powered by a scramjet engine capable of operating at hypersonic speeds (above Mach 5, or five times the speed of sound). The X-43A is powered by a revolutionary air-breathing supersonic-combustion ramjet or "scramjet" engine. In a combined research effort involving Dryden, Langley, and several industry partners, NASA demonstrated the value of its X-43A hypersonic research aircraft, as it became the first air-breathing, unpiloted, scramjet-powered plane to fly freely by itself. The March 27 flight, originating from NASA's Dryden Flight Research Center, began with the Agency's B-52B launch aircraft carrying the X-43A out to the test range over the Pacific Ocean off the California coast. The X-43A was boosted up to its test altitude of about 95,000 feet, where it separated from its modified Pegasus booster and flew freely under its own power. Two very significant aviation milestones occurred during this test flight: first, controlled accelerating flight at Mach 7 under scramjet power, and second, the successful stage separation at high dynamic pressure of two non-axisymmetric vehicles. To top it all off, the flight resulted in the setting of a new aeronautical speed record. The X-43A reached a speed of over Mach 7, or about 5,000 miles per hour faster than any known aircraft powered by an air-breathing engine has ever flown. |
Photo Date |
March 27, 2004 |
|
Photo Description |
Employees atop NASA Dryden's main building celebrate the return flyby of the B-52B aircraft after it launched the second X-43A aircraft on its successful flight. |
Project Description |
The high-risk, high-payoff X-43A flights are the first actual flight tests of an aircraft powered by a scramjet engine capable of operating at hypersonic speeds (above Mach 5, or five times the speed of sound). The X-43A is powered by a revolutionary air-breathing supersonic-combustion ramjet or "scramjet" engine. In a combined research effort involving Dryden, Langley, and several industry partners, NASA demonstrated the value of its X-43A hypersonic research aircraft, as it became the first air-breathing, unpiloted, scramjet-powered plane to fly freely by itself. The March 27 flight, originating from NASA's Dryden Flight Research Center, began with the Agency's B-52B launch aircraft carrying the X-43A out to the test range over the Pacific Ocean off the California coast. The X-43A was boosted up to its test altitude of about 95,000 feet, where it separated from its modified Pegasus booster and flew freely under its own power. Two very significant aviation milestones occurred during this test flight: first, controlled accelerating flight at Mach 7 under scramjet power, and second, the successful stage separation at high dynamic pressure of two non-axisymmetric vehicles. To top it all off, the flight resulted in the setting of a new aeronautical speed record. The X-43A reached a speed of over Mach 7, or about 5,000 miles per hour faster than any known aircraft powered by an air-breathing engine has ever flown. |
Photo Date |
March 27, 2004 |
|
Photo Description |
The second X-43A hypersonic research aircraft and its modified Pegasus booster rocket left the runway, carried aloft by NASA's B-52B launch aircraft from the NASA Dryden Flight Research Center at Edwards Air Force Base, Calif., on March 27, 2004. About an hour later the Pegasus booster was launched from the B-52 to accelerate the X-43A to its intended speed of Mach 7. |
Project Description |
The high-risk, unpiloted X-43A flights are the first actual flight tests of an aircraft powered by a scramjet engine capable of operating at hypersonic speeds (above Mach 5, or five times the speed of sound). The X-43A is powered by a revolutionary air-breathing supersonic-combustion ramjet or "scramjet" engine. In a combined research effort involving Dryden, Langley, and several industry partners, NASA demonstrated the value of its X-43A hypersonic research aircraft, as it became the first air-breathing, unpiloted, scramjet-powered plane to fly freely by itself. The March 27 flight, originating from NASA's Dryden Flight Research Center, began with the Agency's B-52B launch aircraft carrying the X-43A out to the test range over the Pacific Ocean off the California coast. The X-43A was boosted up to its test altitude of about 95,000 feet, where it separated from its modified Pegasus booster and flew freely under its own power. Two very significant aviation milestones occurred during this test flight: first, controlled accelerating flight at Mach 7 under scramjet power, and second, the successful stage separation at high dynamic pressure of two non-axisymmetric vehicles. To top it all off, the flight resulted in the setting of a new aeronautical speed record. The X-43A reached a speed of over Mach 7, or about 5,000 miles per hour faster than any known aircraft powered by an air-breathing engine has ever flown. |
Photo Date |
March 27, 2004 |
|
Photo Description |
The second X-43A hypersonic research aircraft and its modified Pegasus booster rocket left the runway, carried aloft by NASA's B-52B launch aircraft from the NASA Dryden Flight Research Center at Edwards Air Force Base, Calif., on March 27, 2004. About an hour later the Pegasus booster was launched from the B-52 to accelerate the X-43A to its intended speed of Mach 7. |
Project Description |
The high-risk, unpiloted X-43A flights are the first actual flight tests of an aircraft powered by a scramjet engine capable of operating at hypersonic speeds (above Mach 5, or five times the speed of sound). The X-43A is powered by a revolutionary air-breathing supersonic-combustion ramjet or "scramjet" engine. In a combined research effort involving Dryden, Langley, and several industry partners, NASA demonstrated the value of its X-43A hypersonic research aircraft, as it became the first air-breathing, unpiloted, scramjet-powered plane to fly freely by itself. The March 27 flight, originating from NASA's Dryden Flight Research Center, began with the Agency's B-52B launch aircraft carrying the X-43A out to the test range over the Pacific Ocean off the California coast. The X-43A was boosted up to its test altitude of about 95,000 feet, where it separated from its modified Pegasus booster and flew freely under its own power. Two very significant aviation milestones occurred during this test flight: first, controlled accelerating flight at Mach 7 under scramjet power, and second, the successful stage separation at high dynamic pressure of two non-axisymmetric vehicles. To top it all off, the flight resulted in the setting of a new aeronautical speed record. The X-43A reached a speed of over Mach 7, or about 5,000 miles per hour faster than any known aircraft powered by an air-breathing engine has ever flown. |
Photo Date |
March 27, 2004 |
|
Orion Crew Module Model
A half-scale model of the Or
9/4/09
Description |
A half-scale model of the Orion Crew Module is lifted at the Landing and Impact Research (LandIR) Facility Tuesday, Sept. 22, at NASA Langley Research Center in preparation for a pendulum swing test where it will land on Kennedy Space Center simulated sand. The test helps engineers understand how a contingency land landing on sand would impact the crew module after a launch pad abort scenario. Credit: NASA/Sean Smith |
Date |
9/4/09 |
|
HL-10 cockpit
Photo Description |
Cockpit of the HL-10 lifting body. |
Project Description |
The HL-10 was one of five heavyweight lifting-body designs flown at NASA's Flight Research Center (FRC--later Dryden Flight Research Center), Edwards, California, from July 1966 to November 1975 to study and validate the concept of safely maneuvering and landing a low lift-over-drag vehicle designed for reentry from space. Northrop Corporation built the HL-10 and M2-F2, the first two of the fleet of "heavy" lifting bodies flown by the NASA Flight Research Center. The contract for construction of the HL-10 and the M2-F2 was $1.8 million. "HL" stands for horizontal landing, and "10" refers to the tenth design studied by engineers at NASA's Langley Research Center, Hampton, Va. After delivery to NASA in January 1966, the HL-10 made its first flight on Dec. 22, 1966, with research pilot Bruce Peterson in the cockpit. Although an XLR-11 rocket engine was installed in the vehicle, the first 11 drop flights from the B-52 launch aircraft were powerless glide flights to assess handling qualities, stability, and control. In the end, the HL-10 was judged to be the best handling of the three original heavy-weight lifting bodies (M2-F2/F3, HL-10, X-24A). The HL-10 was flown 37 times during the lifting body research program and logged the highest altitude and fastest speed in the Lifting Body program. On Feb. 18, 1970, Air Force test pilot Peter Hoag piloted the HL-10 to Mach 1.86 (1,228 mph). Nine days later, NASA pilot Bill Dana flew the vehicle to 90,030 feet, which became the highest altitude reached in the program. Some new and different lessons were learned through the successful flight testing of the HL-10. These lessons, when combined with information from it's sister ship, the M2-F2/F3, provided an excellent starting point for designers of future entry vehicles, including the Space Shuttle. |
Photo Date |
October 30, 1967 |
|
HL-10 on lakebed with B-52 f
Photo Description |
NASA research pilot Bill Dana takes a moment to watch NASA's NB-52B cruise overhead after a research flight in the HL-10. On the left, John Reeves can be seen at the cockpit of the lifting body. |
Project Description |
The HL-10 was one of five heavyweight lifting-body designs flown at NASA's Flight Research Center (FRC--later Dryden Flight Research Center), Edwards, California, from July 1966 to November 1975 to study and validate the concept of safely maneuvering and landing a low lift-over-drag vehicle designed for reentry from space. Northrop Corporation built the HL-10 and M2-F2, the first two of the fleet of "heavy" lifting bodies flown by the NASA Flight Research Center. The contract for construction of the HL-10 and the M2-F2 was $1.8 million. "HL" stands for horizontal landing, and "10" refers to the tenth design studied by engineers at NASA's Langley Research Center, Hampton, Va. After delivery to NASA in January 1966, the HL-10 made its first flight on Dec. 22, 1966, with research pilot Bruce Peterson in the cockpit. Although an XLR-11 rocket engine was installed in the vehicle, the first 11 drop flights from the B-52 launch aircraft were powerless glide flights to assess handling qualities, stability, and control. In the end, the HL-10 was judged to be the best handling of the three original heavy-weight lifting bodies (M2-F2/F3, HL-10, X-24A). The HL-10 was flown 37 times during the lifting body research program and logged the highest altitude and fastest speed in the Lifting Body program. On Feb. 18, 1970, Air Force test pilot Peter Hoag piloted the HL-10 to Mach 1.86 (1,228 mph). Nine days later, NASA pilot Bill Dana flew the vehicle to 90,030 feet, which became the highest altitude reached in the program. Some new and different lessons were learned through the successful flight testing of the HL-10. These lessons, when combined with information from it's sister ship, the M2-F2/F3, provided an excellent starting point for designers of future entry vehicles, including the Space Shuttle. |
Photo Date |
May 20, 1969 |
|
2009 FIRST Robotics Competit
Rick Mangum and Julia Thomps
3/21/09
Description |
Rick Mangum and Julia Thompson are part of the NASA Langley-sponsored FIRST Robotics team, the NASA Knights, that's based at the New Horizons Regional Educational Center that serves six localities near Hampton. The two participated in the Virginia FIRST Robotics regional competition March 19-21 in Richmond. Mangum is one of the team's fabrication mentors and Thompson, a home-schooled student from Gloucester County, is the team captain. FIRST Robotics was founded by inventor Dean Kamen in 1989. He wanted to create a "world where science and technology are celebrated and where young people dream of becoming science and technology heroes." Credit: NASA/Sean Smith |
Date |
3/21/09 |
|
Penn State's NATIVE Mobile R
On July 13, Pennsylvania Sta
8/3/09
Description |
On July 13, Pennsylvania State University's Dr. Anne Thompson arrived at NASA Langley with her research team to set up their NATIVE (Nittany Atmospheric Trailer) Integrated Validation Experiment) mobile research facility. During their stay, the researchers will be measuring air quality from the trailer in support of NASA's GEO-CAPE (Geostationary Coastal and Air Pollution Events) mission, a next-generation Earth-observing satellite. The NATIVE facility will use its suite of instruments and data analysis tools to make local measurements of gases that are key to tracking pollution, such as carbon monoxide, ozone, nitrogen oxides and sulfur dioxide. Credit: NASA/Sean Smith |
Date |
8/3/09 |
|
NACA Aircraft in hangar 1953
Project Description |
The Dryden Flight Research Center, NASA's premier installation for aeronautical flight research, celebrated its 50th anniversary in 1996. Dryden is the "Center of Excellence" for atmospheric flight operations. The Center's charter is to research, develop, verify, and transfer advanced aeronautics, space, and related technologies. It is located at Edwards, Calif., on the western edge of the Mojave Desert, 80 miles north of Los Angeles. Dryden's history dates back to the early fall of 1946, when a group of five aeronautical engineers arrived at what is now Edwards from the NACA's Langley Memorial Aeronautical Laboratory, Hampton, Va. Their goal was to prepare for the X-l supersonic research flights in a joint NACA-U.S. Army Air Forces-Bell Aircraft Corp. program. NACA--the National Advisory Committee for Aeronautics--was the predecessor of today's NASA. Since the days of the X-l, the first aircraft to fly faster than the speed of sound, the installation has grown in size and significance and is associated with many important developments in aviation -- supersonic and hypersonic flight, wingless lifting bodies, digital fly-by-wire, supercritical and forward-swept wings, and the space shuttles. Its name has changed many times over the years. From 14 November 1949 to 1 July 1954 it bore the name NACA High-Speed Flight Research Station. |
Photo Date |
April 27, 1953 |
|
F-8 DFBW on-board electronic
Photo Description |
The Apollo hardware jammed into the F-8C. The computer is partially visible in the avionics bay at the top of the fuselage behind the cockpit. Note the display and keyboard unit in the gun bay. To carry the computers and other equipment, the F-8 DFBW team removed the aircraft's guns and ammunition boxes. |
Project Description |
The F-8 Digital Fly-By-Wire (DFBW) flight research project validated the principal concepts of all-electric flight control systems now used on nearly all modern high-performance aircraft and on military and civilian transports. The first flight of the 13-year project was on May 25, 1972, with research pilot Gary E. Krier at the controls of a modified F-8C Crusader that served as the testbed for the fly-by-wire technologies. The project was a joint effort between the NASA Flight Research Center, Edwards, California, (now the Dryden Flight Research Center) and Langley Research Center. It included a total of 211 flights. The last flight was December 16, 1985, with Dryden research pilot Ed Schneider at the controls. The F-8 DFBW system was the forerunner of current fly-by-wire systems used in the space shuttles and on today?s military and civil aircraft to make them safer, more maneuverable, and more efficient. Electronic fly-by-wire systems replaced older hydraulic control systems, freeing designers to design aircraft with reduced in-flight stability. Fly-by-wire systems are safer because of their redundancies. They are more maneuverable because computers can command more frequent adjustments than a human pilot can. For airliners, computerized control ensures a smoother ride than a human pilot alone can provide. Digital-fly-by-wire is more efficient because it is lighter and takes up less space than the hydraulic systems it replaced. This either reduces the fuel required to fly or increases the number of passengers or pounds of cargo the aircraft can carry. Digital fly-by-wire is currently used in a variety of aircraft ranging from F/A-18 fighters to the Boeing 777. The DFBW research program is considered one of the most significant and most successful NASA aeronautical programs since the inception of the agency. F-8 aircraft were built originally for the U.S. Navy by LTV Aerospace of Dallas, Texas. The aircraft had a wingspan of 35 feet, 2 inches, was 54 feet, 6 inches long, and was powered by a Pratt & Whitney J57 turbojet engine. |
Photo Date |
June 18, 1971 |
|
Lockheed Electra - aerial vi
Title |
Lockheed Electra - aerial view in flight |
Description |
This shot shows the National Science Foundation Lockheed Electra in a climbing right-hand turn, the video clip runs 14 seconds in length. On Mar. 24, 1998, an L-188 Electra aircraft owned by the National Science Foundation, Arlington, Virginia, and operated by the National Center for Atmospheric Research, Boulder, Colorado, flew near Boulder with an Airborne Coherent LiDAR (Light Detection and Ranging) for Advanced In-flight Measurement. This aircraft was on its first flight to test its ability to detect previously invisible forms of clear air turbulence. Coherent Technologies Inc., Lafayette, Colorado, built the LiDAR device for the NASA Dryden Flight Research Center, Edwards, California. NASA Dryden participated in the effort as part of the NASA Aviation Safety Program, for which the lead center was Langley Research Center, Hampton, Virginia. Results of the test indicated that the device did successfully detect the clear air turbulence. |
Date |
01.01.1999 |
|
Lockheed Electra - animation
Title |
Lockheed Electra - animation showing air turbulence detection |
Description |
On Mar. 24, 1998, an L-188 Electra aircraft owned by the National Science Foundation, Arlington, Virginia, and operated by the National Center for Atmospheric Research, Boulder, Colorado, flew near Boulder with an Airborne Coherent LiDAR (Light Detection and Ranging) for Advanced In-flight Measurement. This aircraft was on its first flight to test its ability to detect previously invisible forms of clear air turbulence. Coherent Technologies Inc., Lafayette, Colorado, built the LiDAR device for the NASA Dryden Flight Research Center, Edwards, California. NASA Dryden participated in the effort as part of the NASA Aviation Safety Program, for which the lead center was Langley Research Center, Hampton, Virginia. Results of the test indicated that the device did successfully detect the clear air turbulence. Computer animation of the clear air turbulence (CAT) detection system known as the "Airborne Coherent LiDAR for Advanced In-flight Measurement" was tested aboard the National Science Foundation L-188 Lockheed Electra. |
Date |
01.01.1999 |
|
Lockheed Electra - takeoff f
Title |
Lockheed Electra - takeoff from runway |
Description |
This 15-second movie clip shows the National Science Foundation Lockheed Electra rotate, lift off, and stow its landing gear on takeoff. On March 24, 1998, an L-188 Electra aircraft owned by the National Science Foundation, Arlington, Virginia and operated by the National Center for Atmospheric Research, Boulder, Colorado, flew near Boulder with an Airborne Coherent LiDAR (Light Detection and Ranging) for Advanced In-flight Measurement. This aircraft was on its first flight to test its ability to detect previously invisible forms of clear air turbulence. Coherent Technologies Inc., Lafayette, Colorado, built the LiDAR device for the NASA Dryden Flight Research Center, Edwards, California. NASA Dryden participated in this effort as part of the NASA Aviation Safety Program, for which the lead center was Langley Research Center, Hampton, Virginia. Results of the test indicated that the device did successfully detect the clear air turbulence. |
Date |
01.01.1999 |
|
X-5 on Ramp - Side View
Photo Description |
This NACA High-Speed Flight Research Station photograph of the X-5 was taken at the South Base of Edwards Air Force Base. The photograph shows the X-5 on the ramp in-front of the NACA hangar. |
Project Description |
The Bell, X-5 was flight tested at the NACA High-Speed Flight Research Station (now the NASA Dryden Flight Research Center, Edwards, California) from 1952 to 1955. The X-5 was the first aircraft capable of sweeping its wings in flight. It helped provide data about wing-sweep at angles of up to 60 degrees at subsonic and transonic speeds. There were two X-5 vehicles. Ship 1 was flown at the NACA High-Speed Flight Research Station (High-Speed Flight Station, as it was redesignated in 1954) from 1951 to 1955. Ship 2 was operated by Bell and the U.S. Air Force and was lost in a spin accident in 1953. Following the conclusion of the contractor?s test program, the X-5 was grounded for installation of a NACA instrument package. The Air Force conducted a short, six-flight, evaluation program. Since the Air Force evaluation program included data collection, it was considered as part of the overall NACA effort and flights were logged as AF/NACA. In the NACA test program, the X-5 demonstrated severe stall-spin instability. The X-5 was also used as a chase plane for other research aircraft because it could vary its flying characteristics to suit the airplane it was chasing. Ship 1 flew a total of 133 flights during its three years of service. In spite of the problems with the aircraft, the X-5 provided a significant full-scale verification of NACA wind-tunnel predictions for reduced drag and improved performance that resulted from this configuration?s increasing the wing sweep as the speed of the aircraft approached the speed of sound. The X-5 flight tests provided some of the design data for the Air Force F-111 and Navy F-14 tactical aircraft. Although the mechanism by which the X-5 changed its wing sweep made this particular design impractical, development of a viable variable-sweep aircraft had to await Langley Aeronautical Laboratory?s concept of an outboard wing pivot in the mid-1950s. (Langley was a NACA research laboratory in Hampton, Virginia.) The X-5 was a single seat aircraft powered by an Allison J-35-A-17A jet engine. It was 33.33 feet long with a wingspan of 20.9 feet (with the wings swept back at an angle of 60 degrees) to 33.5 feet (with the wings unswept). When fully fueled, the X-5 weighed 9,875 pounds. |
Photo Date |
1952 |
|
X-5 on Ramp
Photo Description |
This NACA High-Speed Flight Research Station photograph of the X-5 was taken at the South Base of Edwards Air Force Base in 1952. The photograph is a left side view of the aircraft on the ramp. |
Project Description |
The Bell, X-5 was flight tested at the NACA High-Speed Flight Research Station (now the NASA Dryden Flight Research Center, Edwards, California) from 1952 to 1955. The X-5 was the first aircraft capable of sweeping its wings in flight. It helped provide data about wing-sweep at angles of up to 60 degrees at subsonic and transonic speeds. There were two X-5 vehicles. Ship 1 was flown at the NACA High-Speed Flight Research Station (High-Speed Flight Station, as it was redesignated in 1954) from 1951 to 1955. Ship 2 was operated by Bell and the U.S. Air Force and was lost in a spin accident in 1953. Following the conclusion of the contractor?s test program, the X-5 was grounded for installation of a NACA instrument package. The Air Force conducted a short, six-flight, evaluation program. Since the Air Force evaluation program included data collection, it was considered as part of the overall NACA effort and flights were logged as AF/NACA. In the NACA test program, the X-5 demonstrated severe stall-spin instability. The X-5 was also used as a chase plane for other research aircraft because it could vary its flying characteristics to suit the airplane it was chasing. Ship 1 flew a total of 133 flights during its three years of service. In spite of the problems with the aircraft, the X-5 provided a significant full-scale verification of NACA wind-tunnel predictions for reduced drag and improved performance that resulted from this configuration?s increasing the wing sweep as the speed of the aircraft approached the speed of sound. The X-5 flight tests provided some of the design data for the Air Force F-111 and Navy F-14 tactical aircraft. Although the mechanism by which the X-5 changed its wing sweep made this particular design impractical, development of a viable variable-sweep aircraft had to await Langley Aeronautical Laboratory?s concept of an outboard wing pivot in the mid-1950s. (Langley was a NACA research laboratory in Hampton, Virginia.) The X-5 was a single seat aircraft powered by an Allison J-35-A-17A jet engine. It was 33.33 feet long with a wingspan of 20.9 feet (with the wings swept back at an angle of 60 degrees) to 33.5 feet (with the wings unswept). When fully fueled, the X-5 weighed 9,875 pounds. |
Photo Date |
January 1952 |
|
X-5 Multiple Exposure Photo
Photo Description |
This NACA High-Speed Flight Research Station photograph of the X-5 was taken at the South Base of Edwards Air Force Base. The photograph, a multiple exposure, illustrates the X-5's variably swept wing capability. |
Project Description |
The Bell, X-5 was flight tested at the NACA High-Speed Flight Research Station (now the NASA Dryden Flight Research Center, Edwards, California) from 1952 to 1955. The X-5 was the first aircraft capable of sweeping its wings in flight. It helped provide data about wing-sweep at angles of up to 60 degrees at subsonic and transonic speeds. There were two X-5 vehicles. Ship 1 was flown at the NACA High-Speed Flight Research Station (High-Speed Flight Station, as it was redesignated in 1954) from 1951 to 1955. Ship 2 was operated by Bell and the U.S. Air Force and was lost in a spin accident in 1953. Following the conclusion of the contractor?s test program, the X-5 was grounded for installation of a NACA instrument package. The Air Force conducted a short, six-flight, evaluation program. Since the Air Force evaluation program included data collection, it was considered as part of the overall NACA effort and flights were logged as AF/NACA. In the NACA test program, the X-5 demonstrated severe stall-spin instability. The X-5 was also used as a chase plane for other research aircraft because it could vary its flying characteristics to suit the airplane it was chasing. Ship 1 flew a total of 133 flights during its three years of service. In spite of the problems with the aircraft, the X-5 provided a significant full-scale verification of NACA wind-tunnel predictions for reduced drag and improved performance that resulted from this configuration?s increasing the wing sweep as the speed of the aircraft approached the speed of sound. The X-5 flight tests provided some of the design data for the Air Force F-111 and Navy F-14 tactical aircraft. Although the mechanism by which the X-5 changed its wing sweep made this particular design impractical, development of a viable variable-sweep aircraft had to await Langley Aeronautical Laboratory?s concept of an outboard wing pivot in the mid-1950s. (Langley was a NACA research laboratory in Hampton, Virginia.) The X-5 was a single seat aircraft powered by an Allison J-35-A-17A jet engine. It was 33.33 feet long with a wingspan of 20.9 feet (with the wings swept back at an angle of 60 degrees) to 33.5 feet (with the wings unswept). When fully fueled, the X-5 weighed 9,875 pounds. |
Photo Date |
23 September 1952 |
|
X-5
Photo Description |
This NACA High-Speed Flight Research Station photograph of the X-5 was taken at Edwards Air Force Base in the mid 1950s. The photograph shows the aircraft in flight with the wings swept back. |
Project Description |
The Bell, X-5 was flight tested at the NACA High-Speed Flight Research Station (now the NASA Dryden Flight Research Center, Edwards, California) from 1952 to 1955. The X-5 was the first aircraft capable of sweeping its wings in flight. It helped provide data about wing-sweep at angles of up to 60 degrees at subsonic and transonic speeds. There were two X-5 vehicles. Ship 1 was flown at the NACA High-Speed Flight Research Station (High-Speed Flight Station, as it was redesignated in 1954) from 1951 to 1955. Ship 2 was operated by Bell and the U.S. Air Force and was lost in a spin accident in 1953. Following the conclusion of the contractor?s test program, the X-5 was grounded for installation of a NACA instrument package. The Air Force conducted a short, six-flight, evaluation program. Since the Air Force evaluation program included data collection, it was considered as part of the overall NACA effort and flights were logged as AF/NACA. In the NACA test program, the X-5 demonstrated severe stall-spin instability. The X-5 was also used as a chase plane for other research aircraft because it could vary its flying characteristics to suit the airplane it was chasing. Ship 1 flew a total of 133 flights during its three years of service. In spite of the problems with the aircraft, the X-5 provided a significant full-scale verification of NACA wind-tunnel predictions for reduced drag and improved performance that resulted from this configuration?s increasing the wing sweep as the speed of the aircraft approached the speed of sound. The X-5 flight tests provided some of the design data for the Air Force F-111 and Navy F-14 tactical aircraft. Although the mechanism by which the X-5 changed its wing sweep made this particular design impractical, development of a viable variable-sweep aircraft had to await Langley Aeronautical Laboratory?s concept of an outboard wing pivot in the mid-1950s. (Langley was a NACA research laboratory in Hampton, Virginia.) The X-5 was a single seat aircraft powered by an Allison J-35-A-17A jet engine. It was 33.33 feet long with a wingspan of 20.9 feet (with the wings swept back at an angle of 60 degrees) to 33.5 feet (with the wings unswept). When fully fueled, the X-5 weighed 9,875 pounds. |
Photo Date |
1957 |
|
Hyper-X and Pegasus Launch V
Title |
Hyper-X and Pegasus Launch Vehicle: A Three-Foot Model of the Hypersonic Experimental Research Vehic |
Description |
The configuration of the X-43A Hypersonic Experimental Research Vehicle, or Hyper-X, attached to a Pegasus launch vehicle is displayed in this three-foot-long model at NASA's Dryden Flight Research Center, Edwards, California. Hyper-X, the flight vehicle for which is designated as X-43A, is an experimental flight-research program seeking to demonstrate airframe-integrated, "air-breathing" engine technologies that promise to increase payload capacity for future vehicles, including hypersonic aircraft (faster than Mach 5) and reusable space launchers. This multiyear program is currently underway at NASA Dryden Flight Research Center, Edwards, California. The Hyper-X schedule calls for its first flight later this year (2000). Hyper-X is a joint program, with Dryden sharing responsibility with NASA's Langley Research Center, Hampton, Virginia. Dryden's primary role is to fly three unpiloted X-43A research vehicles to validate engine technologies and hypersonic design tools as well as the hypersonic test facility at Langley. Langley manages the program and leads the technology development effort. The Hyper-X Program seeks to significantly expand the speed boundaries of air-breathing propulsion by being the first aircraft to demonstrate an airframe-integrated, scramjet-powered free flight. Scramjets (supersonic-combustion ramjets) are ramjet engines in which the airflow through the whole engine remains supersonic. Scramjet technology is challenging because only limited testing can be performed in ground facilities. Long duration, full-scale testing requires flight research. Scramjet engines are air-breathing, capturing their oxygen from the atmosphere. Current spacecraft, such as the Space Shuttle, are rocket powered, so they must carry both fuel and oxygen for propulsion. Scramjet technology-based vehicles need to carry only fuel. By eliminating the need to carry oxygen, future hypersonic vehicles will be able to carry heavier payloads. Another unique aspect of the X-43A vehicle is the airframe integration. The body of the vehicle itself forms critical elements of the engine. The forebody acts as part of the intake for airflow and the aft section serves as the nozzle. The X-43A vehicles were manufactured by Micro Craft, Inc., Tullahoma, Tennessee. Orbital Sciences Corporation, Chandler, Arizona, built the Pegasus rocket booster used to launch the X-43 vehicles. For the Dryden research flights, the Pegasus rocket booster and attached X-43 will be air launched by Dryden's B-52 "Mothership." After release from the B-52, the booster will accelerate the X-43A vehicle to the established test conditions (Mach 7 to 10) at an altitude of approximately 100,000 feet where the X-43 will separate from the booster and fly under its own power and preprogrammed control. |
Date |
05.01.1997 |
|
Hyper-X and Pegasus Launch V
Title |
Hyper-X and Pegasus Launch Vehicle: A Three-Foot Model of the Hypersonic Experimental Research Vehic |
Description |
A close-up view of the X-43A Hypersonic Experimental Research Vehicle, or Hyper-X, portion of a three-foot-long model of the vehicle/booster combination at NASA's Dryden Flight Research Center, Edwards, California. Hyper-X, the flight vehicle for which is designated as X-43A, is an experimental flight-research program seeking to demonstrate airframe-integrated, "air-breathing" engine technologies that promise to increase payload capacity for future vehicles, including hypersonic aircraft (faster than Mach 5) and reusable space launchers. This multiyear program is currently underway at NASA Dryden Flight Research Center, Edwards, California. The Hyper-X schedule calls for its first flight later this year (2000). Hyper-X is a joint program, with Dryden sharing responsibility with NASA's Langley Research Center, Hampton, Virginia. Dryden's primary role is to fly three unpiloted X-43A research vehicles to validate engine technologies and hypersonic design tools as well as the hypersonic test facility at Langley. Langley manages the program and leads the technology development effort. The Hyper-X Program seeks to significantly expand the speed boundaries of air-breathing propulsion by being the first aircraft to demonstrate an airframe-integrated, scramjet-powered free flight. Scramjets (supersonic-combustion ramjets) are ramjet engines in which the airflow through the whole engine remains supersonic. Scramjet technology is challenging because only limited testing can be performed in ground facilities. Long duration, full-scale testing requires flight research. Scramjet engines are air-breathing, capturing their oxygen from the atmosphere. Current spacecraft, such as the Space Shuttle, are rocket powered, so they must carry both fuel and oxygen for propulsion. Scramjet technology-based vehicles need to carry only fuel. By eliminating the need to carry oxygen, future hypersonic vehicles will be able to carry heavier payloads. Another unique aspect of the X-43A vehicle is the airframe integration. The body of the vehicle itself forms critical elements of the engine. The forebody acts as part of the intake for airflow and the aft section serves as the nozzle. The X-43A vehicles were manufactured by Micro Craft, Inc., Tullahoma, Tennessee. Orbital Sciences Corporation, Chandler, Arizona, built the Pegasus rocket booster used to launch the X-43 vehicles. For the Dryden research flights, the Pegasus rocket booster and attached X-43 will be air launched by Dryden's B-52 "Mothership." After release from the B-52, the booster will accelerate the X-43A vehicle to the established test conditions (Mach 7 to 10) at an altitude of approximately 100,000 feet where the X-43 will separate from the booster and fly under its own power and preprogrammed control. |
Date |
05.01.1997 |
|
Hyper-X and Pegasus Launch V
Title |
Hyper-X and Pegasus Launch Vehicle: A Three-Foot Model of the Hypersonic Experimental Research Vehic |
Description |
The configuration of the X-43A Hypersonic Experimental Research Vehicle, or Hyper-X, attached to a Pegasus launch vehicle is displayed in this side view of a three-foot-long model of the vehicle/booster combination at NASA's Dryden Flight Research Center, Edwards, California. Hyper-X, the flight vehicle for which is designated as X-43A, is an experimental flight-research program seeking to demonstrate airframe-integrated, "air-breathing" engine technologies that promise to increase payload capacity for future vehicles, including hypersonic aircraft (faster than Mach 5) and reusable space launchers. This multiyear program is currently underway at NASA Dryden Flight Research Center, Edwards, California. The Hyper-X schedule calls for its first flight later this year (2000). Hyper-X is a joint program, with Dryden sharing responsibility with NASA's Langley Research Center, Hampton, Virginia. Dryden's primary role is to fly three unpiloted X-43A research vehicles to validate engine technologies and hypersonic design tools as well as the hypersonic test facility at Langley. Langley manages the program and leads the technology development effort. The Hyper-X Program seeks to significantly expand the speed boundaries of air-breathing propulsion by being the first aircraft to demonstrate an airframe-integrated, scramjet-powered free flight. Scramjets (supersonic-combustion ramjets) are ramjet engines in which the airflow through the whole engine remains supersonic. Scramjet technology is challenging because only limited testing can be performed in ground facilities. Long duration, full-scale testing requires flight research. Scramjet engines are air-breathing, capturing their oxygen from the atmosphere. Current spacecraft, such as the Space Shuttle, are rocket powered, so they must carry both fuel and oxygen for propulsion. Scramjet technology-based vehicles need to carry only fuel. By eliminating the need to carry oxygen, future hypersonic vehicles will be able to carry heavier payloads. Another unique aspect of the X-43A vehicle is the airframe integration. The body of the vehicle itself forms critical elements of the engine. The forebody acts as part of the intake for airflow and the aft section serves as the nozzle. The X-43A vehicles were manufactured by Micro Craft, Inc., Tullahoma, Tennessee. Orbital Sciences Corporation, Chandler, Arizona, built the Pegasus rocket booster used to launch the X-43 vehicles. For the Dryden research flights, the Pegasus rocket booster and attached X-43 will be air launched by Dryden's B-52 "Mothership." After release from the B-52, the booster will accelerate the X-43A vehicle to the established test conditions (Mach 7 to 10) at an altitude of approximately 100,000 feet where the X-43 will separate from the booster and fly under its own power and preprogrammed control. |
Date |
05.01.1997 |
|
Hyper-X and Pegasus Launch V
Title |
Hyper-X and Pegasus Launch Vehicle: A Three-Foot Model of the Hypersonic Experimental Research Vehic |
Description |
The configuration of the X-43A Hypersonic Experimental Research Vehicle, or Hyper-X, attached to a Pegasus launch vehicle is displayed in this three-foot-long model at NASA's Dryden Flight Research Center, Edwards, California. Hyper-X, the flight vehicle for which is designated as X-43A, is an experimental flight-research program seeking to demonstrate airframe-integrated, "air-breathing" engine technologies that promise to increase payload capacity for future vehicles, including hypersonic aircraft (faster than Mach 5) and reusable space launchers. This multiyear program is currently underway at NASA Dryden Flight Research Center, Edwards, California. The Hyper-X schedule calls for its first flight later this year (2000). Hyper-X is a joint program, with Dryden sharing responsibility with NASA's Langley Research Center, Hampton, Virginia. Dryden's primary role is to fly three unpiloted X-43A research vehicles to validate engine technologies and hypersonic design tools as well as the hypersonic test facility at Langley. Langley manages the program and leads the technology development effort. The Hyper-X Program seeks to significantly expand the speed boundaries of air-breathing propulsion by being the first aircraft to demonstrate an airframe-integrated, scramjet-powered free flight. Scramjets (supersonic-combustion ramjets) are ramjet engines in which the airflow through the whole engine remains supersonic. Scramjet technology is challenging because only limited testing can be performed in ground facilities. Long duration, full-scale testing requires flight research. Scramjet engines are air-breathing, capturing their oxygen from the atmosphere. Current spacecraft, such as the Space Shuttle, are rocket powered, so they must carry both fuel and oxygen for propulsion. Scramjet technology-based vehicles need to carry only fuel. By eliminating the need to carry oxygen, future hypersonic vehicles will be able to carry heavier payloads. Another unique aspect of the X-43A vehicle is the airframe integration. The body of the vehicle itself forms critical elements of the engine. The forebody acts as part of the intake for airflow and the aft section serves as the nozzle. The X-43A vehicles were manufactured by Micro Craft, Inc., Tullahoma, Tennessee. Orbital Sciences Corporation, Chandler, Arizona, built the Pegasus rocket booster used to launch the X-43 vehicles. For the Dryden research flights, the Pegasus rocket booster and attached X-43 will be air launched by Dryden's B-52 "Mothership." After release from the B-52, the booster will accelerate the X-43A vehicle to the established test conditions (Mach 7 to 10) at an altitude of approximately 100,000 feet where the X-43 will separate from the booster and fly under its own power and preprogrammed control. |
Date |
05.01.1997 |
|
Hyper-X and Pegasus Launch V
Title |
Hyper-X and Pegasus Launch Vehicle: A Three-Foot Model of the Hypersonic Experimental Research Vehic |
Description |
The configuration of the X-43A Hypersonic Experimental Research Vehicle, or Hyper-X, attached to a Pegasus launch vehicle is displayed in this three-foot-long model at NASA's Dryden Flight Research Center, Edwards, California. Hyper-X, the flight vehicle for which is designated as X-43A, is an experimental flight-research program seeking to demonstrate airframe-integrated, "air-breathing" engine technologies that promise to increase payload capacity for future vehicles, including hypersonic aircraft (faster than Mach 5) and reusable space launchers. This multiyear program is currently underway at NASA Dryden Flight Research Center, Edwards, California. The Hyper-X schedule calls for its first flight later this year (2000). Hyper-X is a joint program, with Dryden sharing responsibility with NASA's Langley Research Center, Hampton, Virginia. Dryden's primary role is to fly three unpiloted X-43A research vehicles to validate engine technologies and hypersonic design tools as well as the hypersonic test facility at Langley. Langley manages the program and leads the technology development effort. The Hyper-X Program seeks to significantly expand the speed boundaries of air-breathing propulsion by being the first aircraft to demonstrate an airframe-integrated, scramjet-powered free flight. Scramjets (supersonic-combustion ramjets) are ramjet engines in which the airflow through the whole engine remains supersonic. Scramjet technology is challenging because only limited testing can be performed in ground facilities. Long duration, full-scale testing requires flight research. Scramjet engines are air-breathing, capturing their oxygen from the atmosphere. Current spacecraft, such as the Space Shuttle, are rocket powered, so they must carry both fuel and oxygen for propulsion. Scramjet technology-based vehicles need to carry only fuel. By eliminating the need to carry oxygen, future hypersonic vehicles will be able to carry heavier payloads. Another unique aspect of the X-43A vehicle is the airframe integration. The body of the vehicle itself forms critical elements of the engine. The forebody acts as part of the intake for airflow and the aft section serves as the nozzle. The X-43A vehicles were manufactured by Micro Craft, Inc., Tullahoma, Tennessee. Orbital Sciences Corporation, Chandler, Arizona, built the Pegasus rocket booster used to launch the X-43 vehicles. For the Dryden research flights, the Pegasus rocket booster and attached X-43 will be air launched by Dryden's B-52 "Mothership." After release from the B-52, the booster will accelerate the X-43A vehicle to the established test conditions (Mach 7 to 10) at an altitude of approximately 100,000 feet where the X-43 will separate from the booster and fly under its own power and preprogrammed control. |
Date |
05.01.1997 |
|
Crew Module, Launch Abort Sy
Ares I-X simulated crew modu
2/2/09
Description |
Ares I-X simulated crew module and launch abort system flight hardware arrives at NASA's Kennedy Space Center in Florida. This hardware will complete the nose of the rocket. Nearly 150 sensors on the hardware will measure aerodynamic pressure and temperature at the nose of the rocket and contribute to measurements of vehicle acceleration and angle of attack. The data will help NASA understand whether the design is safe and stable in flight, a question that must be answered before astronauts begin traveling into orbit and beyond. Credit: NASA/Sean Smith |
Date |
2/2/09 |
|
B-57B on ramp
Title |
B-57B on ramp |
Description |
A converted Martin B-57B Canberra medium bomber sits on the ramp at the NASA Ames-Dryden Flight Research Facility, Edwards, California. The rugged NASA aircraft was flown by Dryden in the early 1970s to learn more about the atmosphere. Instrumented with a data acquisition system, Dryden pilots measured atmospheric conditions and clear-air turbulence at various altitudes and sampled the upper atmosphere for various aerosols. The research - to give scientists a better understanding of mountain waves, jet streams, convective turbulence, clear-air turbulence, and atmospheric contaminants - was sponsored by NASA's Langley Research Center, the University of Wyoming, and the Department of Transportation. The aircraft was retired from flight status in 1987. In the early 1970s, a Martin B-57B Canberra light bomber was used in several NASA joint flight test programs at the NASA Flight Research Center (now Dryden Flight Research Center) located at Edwards Air Force Base, California. The early 1970s showed a growing interest in continuing atmospheric research. The B-57B was at the NASA Flight Research Center for a joint program with NASA Langley Research Center, Hampton, Virginia and was having a special set of instrumentation installed. Delays in completing the instruments provided an opportunity to support the NASA space program. The B-57B was used in proof-of-concept testing of the Viking Mars landers. The deceleration drop testing part of the program took place at the Joint Parachute Test Facility, El Centro, California. With completion of the Viking parachute tests, the B-57B was flown for measuring and analysis of atmospheric turbulence research in 1974-75 as part of a joint NASA program between the Flight Research Center and Langley Research Center. Additional atmospheric testing provided samples of aerosols for the University of Wyoming and clear-air turbulence data for the Department of Transportation. The aircraft was tested over a span of many years at Edwards Air Force Base by various NASA centers for other types of research. Earlier, in the 1960s, the aircraft was flown at the Flight Research Center by the Lewis Research Center (now the John Glenn Research Center) in support of the newly established NASA Electronics Center in Boston, Massachusetts. Later, in 1982, the B-57B aircraft returned to the Flight Research Center (then the Ames-Dryden Flight Research Facility) for more Langley-sponsored turbulence testing. The atmospheric research conducted using the B-57B Canberra provided information on mountain waves, jet streams, convective turbulence, and clear-air turbulence. |
Date |
01.01.1982 |
|
Photo Description |
NASA's historic B-52 mother ship carried the X-43A and its Pegasus booster rocket on a captive carry flight from Edwards Air Force Base Jan. 26, 2004. The X-43A and its booster remained mated to the B-52 throughout the two-hour flight, intended to check its readiness for launch. The hydrogen-fueled aircraft is autonomous and has a wingspan of approximately 5 feet, measures 12 feet long and weighs about 2,800 pounds. |
Project Description |
The X-43A will ride on the first stage of an Orbital Sciences Corp. Pegasus booster rocket, which will be launched by Dryden's B-52 at about 40,000 feet. For each flight, the booster will accelerate the X-43A research vehicle to the test conditions (Mach 7 or 10) at approximately 100,000 feet, where it will separate from the booster and fly under its own power. In a combined research effort involving Dryden, Langley, and several industry partners, NASA demonstrated the value of its X-43A hypersonic research aircraft, as it became the first air-breathing, unpiloted, scramjet-powered plane to fly freely by itself. The March 27 flight, originating from NASA's Dryden Flight Research Center, began with the Agency's B-52B launch aircraft carrying the X-43A out to the test range over the Pacific Ocean off the California coast. The X-43A was boosted up to its test altitude of about 95,000 feet, where it separated from its modified Pegasus booster and flew freely under its own power. Two very significant aviation milestones occurred during this test flight: first, controlled accelerating flight at Mach 7 under scramjet power, and second, the successful stage separation at high dynamic pressure of two non-axisymmetric vehicles. To top it all off, the flight resulted in the setting of a new aeronautical speed record. The X-43A reached a speed of over Mach 7, or about 5,000 miles per hour faster than any known aircraft powered by an air-breathing engine has ever flown. |
Photo Date |
Jan. 26, 2004 |
|
Photo Description |
NASA's historic B-52 mother ship carried the X-43A and its Pegasus booster rocket on a captive carry flight from Edwards Air Force Base Jan. 26, 2004. The X-43A and its booster remained mated to the B-52 throughout the two-hour flight, intended to check its readiness for launch. The hydrogen-fueled aircraft is autonomous and has a wingspan of approximately 5 feet, measures 12 feet long and weighs about 2,800 pounds. |
Project Description |
The X-43A will ride on the first stage of an Orbital Sciences Corp. Pegasus booster rocket, which will be launched by Dryden's B-52 at about 40,000 feet. For each flight, the booster will accelerate the X-43A research vehicle to the test conditions (Mach 7 or 10) at approximately 100,000 feet, where it will separate from the booster and fly under its own power. In a combined research effort involving Dryden, Langley, and several industry partners, NASA demonstrated the value of its X-43A hypersonic research aircraft, as it became the first air-breathing, unpiloted, scramjet-powered plane to fly freely by itself. The March 27 flight, originating from NASA's Dryden Flight Research Center, began with the Agency's B-52B launch aircraft carrying the X-43A out to the test range over the Pacific Ocean off the California coast. The X-43A was boosted up to its test altitude of about 95,000 feet, where it separated from its modified Pegasus booster and flew freely under its own power. Two very significant aviation milestones occurred during this test flight: first, controlled accelerating flight at Mach 7 under scramjet power, and second, the successful stage separation at high dynamic pressure of two non-axisymmetric vehicles. To top it all off, the flight resulted in the setting of a new aeronautical speed record. The X-43A reached a speed of over Mach 7, or about 5,000 miles per hour faster than any known aircraft powered by an air-breathing engine has ever flown. |
Photo Date |
Jan. 26, 2004 |
|
Photo Description |
NASA's historic B-52 mother ship carried the X-43A and its Pegasus booster rocket on a captive carry flight from Edwards Air Force Base Jan. 26, 2004. The X-43A and its booster remained mated to the B-52 throughout the two-hour flight, intended to check its readiness for launch. The hydrogen-fueled aircraft is autonomous and has a wingspan of approximately 5 feet, measures 12 feet long and weighs about 2,800 pounds. |
Project Description |
The X-43A will ride on the first stage of an Orbital Sciences Corp. Pegasus booster rocket, which will be launched by Dryden's B-52 at about 40,000 feet. For each flight, the booster will accelerate the X-43A research vehicle to the test conditions (Mach 7 or 10) at approximately 100,000 feet, where it will separate from the booster and fly under its own power. In a combined research effort involving Dryden, Langley, and several industry partners, NASA demonstrated the value of its X-43A hypersonic research aircraft, as it became the first air-breathing, unpiloted, scramjet-powered plane to fly freely by itself. The March 27 flight, originating from NASA's Dryden Flight Research Center, began with the Agency's B-52B launch aircraft carrying the X-43A out to the test range over the Pacific Ocean off the California coast. The X-43A was boosted up to its test altitude of about 95,000 feet, where it separated from its modified Pegasus booster and flew freely under its own power. Two very significant aviation milestones occurred during this test flight: first, controlled accelerating flight at Mach 7 under scramjet power, and second, the successful stage separation at high dynamic pressure of two non-axisymmetric vehicles. To top it all off, the flight resulted in the setting of a new aeronautical speed record. The X-43A reached a speed of over Mach 7, or about 5,000 miles per hour faster than any known aircraft powered by an air-breathing engine has ever flown. |
Photo Date |
Jan. 26, 2004 |
|
Photo Description |
The black X-43A rides on the front of a modified Pegasus booster rocket hung from the special pylon under the wing of NASA's B-52B mother ship. The photo was taken during a captive carry flight Jan. 26, 2004 to verify systems before an upcoming launch. |
Project Description |
X-43A will ride on the first stage of an Orbital Sciences Corp., Dulles, Virginia, booster rocket, which will be launched by Dryden's B-52 at about 40,000 feet. For each flight, the booster will accelerate the X-43A research vehicle to the test conditions (Mach 7 or 10) at approximately 100,000 feet, where it will separate from the booster and fly under its own power. Orbital Science's Launch Vehicles Division in Chandler, Arizona. will construct the Hyper-X launch vehicles. In a combined research effort involving Dryden, Langley, and several industry partners, NASA demonstrated the value of its X-43A hypersonic research aircraft, as it became the first air-breathing, unpiloted, scramjet-powered plane to fly freely by itself. The March 27 flight, originating from NASA's Dryden Flight Research Center, began with the Agency's B-52B launch aircraft carrying the X-43A out to the test range over the Pacific Ocean off the California coast. The X-43A was boosted up to its test altitude of about 95,000 feet, where it separated from its modified Pegasus booster and flew freely under its own power. Two very significant aviation milestones occurred during this test flight: first, controlled accelerating flight at Mach 7 under scramjet power, and second, the successful stage separation at high dynamic pressure of two non-axisymmetric vehicles. To top it all off, the flight resulted in the setting of a new aeronautical speed record. The X-43A reached a speed of over Mach 7, or about 5,000 miles per hour faster than any known aircraft powered by an air-breathing engine has ever flown. |
Photo Date |
January 26, 2004 |
|
Dryden staff formed long lin
Long-time NASA Dryden resear
8/29/08
Description |
Long-time NASA Dryden research pilot and former astronaut C. Gordon Fullerton capped an almost 50-year flying career, including more than 38 years with NASA, with a final flight in a NASA F/A-18 on Dec. 21, 2007. Fullerton and Dryden research pilot Jim Smolka flew a 90-minute pilot proficiency formation aerobatics flight with another Dryden F/A-18 and a Dryden T-38 before concluding with two low-level formation flyovers of Dryden before landing. Fullerton was honored with a water-cannon spray arch provided by two fire trucks from the Edwards Air Force Base fire department as he taxied the F/A-18 up to the Dryden ramp, and was then greeted by his wife Marie and several hundred Dryden staff after his final flight. December 21, 2007 NASA / Photo Tom Tschida ED07-0294-44 |
Date |
8/29/08 |
|
F-8 SCW in flight
Photo Description |
The F-8A Supercritical Wing (SCW) aircraft in flight. Dr. Richard T. Whitcomb began work on the supercritical wing in the early 1960s. Although the design was highly efficient in wind-tunnel testing, it was so unusual that few accepted the concept as practical. Larry Loftin of NASA's Langley Research Center in Hampton, VA, said, "We're going to have a flight demonstration. This thing is so different from anything that we've ever done before that nobody's going to touch it with a ten foot pole without somebody going out and flying it." The Navy supplied NASA with an F-8A (Navy Bureau Number 141353/NASA tail number 810), while North American Aviation built the supercritical wing. The SCW team attached it to the stock F-8 fuselage. This 1971 photo shows its original paint finish. Tom McMurtry, who was the lead project pilot, recalled that there was no time or money for a fancier finish. In fact, on the first flight, made on March 9, 1971, the "SCW" on the tail was actually taped on. |
Project Description |
The F-8 Supercritical Wing was a flight research project designed to test a new wing concept designed by Dr. Richard Whitcomb, chief of the Transonic Aerodynamics Branch, Langley Research Center, Hampton, Virginia. Compared to a conventional wing, the supercritical wing (SCW) is flatter on the top and rounder on the bottom with a downward curve at the trailing edge. The Supercritical Wing was designed to delay the formation of and reduce the shock wave over the wing just below and above the speed of sound (transonic region of flight). Delaying the shock wave at these speeds results in less drag. Results of the NASA flight research at the Flight Research Center, Edwards, California, (later renamed the Dryden Flight Research Center) demonstrated that aircraft using the supercritical wing concept would have increased cruising speed, improved fuel efficiency, and greater flight range than those using conventional wings. As a result, supercritical wings are now commonplace on virtually every modern subsonic commercial transport. Results of the NASA project showed the SCW had increased the transonic efficiency of the F-8 as much as 15 percent and proved that passenger transports with supercritical wings, versus conventional wings, could save $78 million (in 1974 dollars) per year for a fleet of 280 200-passenger airliners. The F-8 Supercritical Wing (SCW) project flew from 1970 to 1973. Dryden engineer John McTigue was the first SCW program manager and Tom McMurtry was the lead project pilot. The first SCW flight took place on March 9, 1971. The last flight of the Supercritical wing was on May 23, 1973, with Ron Gerdes at the controls. Original wingspan of the F-8 is 35 feet, 2 inches while the wingspan with the supercritical wing was 43 feet, 1 inch. F-8 aircraft were powered by Pratt & Whitney J57 turbojet engines. The TF-8A Crusader was made available to the NASA Flight Research Center by the U.S. Navy. F-8 jet aircraft were built, originally, by LTV Aerospace, Dallas, Texas. Rockwell International?s North American Aircraft Division received a $1.8 million contract to fabricate the supercritical wing, which was delivered to NASA in December 1969. |
Photo Date |
March 17, 1971 |
|
C-140 JetStar landing on Rog
Image of the Week -- IRVE
WALLOPS ISLAND, Va. -- A suc
8/18/09
Description |
WALLOPS ISLAND, Va. -- A successful NASA flight test has shown that a spacecraft returning to Earth can use an inflatable heat shield to slow and protect itself as it enters the atmosphere at hypersonic speeds. This was the first time anyone has successfully flown an inflatable reentry capsule, according to engineers at NASA's Langley Research Center. The Inflatable Re-entry Vehicle Experiment, or IRVE, was vacuum-packed into a 15-inch diameter payload "shroud" and launched on a small sounding rocket from NASA's Wallops Flight Facility on Wallops Island, Va. Nitrogen inflated the 10-foot (3 m) diameter heat shield, made of several layers of silicone-coated industrial fabric, to a mushroom shape in space several minutes after liftoff. "This was a huge success," said Mary Beth Wusk, IRVE project manager, based at Langley. "IRVE was a small-scale demonstrator. Now that we've proven the concept, we'd like to build more advanced aeroshells capable of handling higher heat rates." The Black Brant 9 rocket took about four minutes to lift the experiment to an altitude of 131 miles (211 km). Less than a minute later it was released from its cover and started inflating on schedule at 124 miles (199.5 km) up. The inflation of the shield took less than 90 seconds. "Everything performed well even into the subsonic range where we weren't sure what to expect," said Neil Cheatwood, IRVE principal investigator and chief scientist for the Hypersonics Project of NASA's Aeronautics Research Mission Directorate's Fundamental Aeronautics Program. "The telemetry looks good. The inflatable bladder held up well." Inflatable heat shields hold promise for future planetary missions, according to researchers. To land more mass on Mars at higher surface elevations, for instance, mission planners need to maximize the drag area of the entry system. The larger the diameter of the aeroshell, the bigger the payload can be. Credit: NASA/Sean Smith |
Date |
8/18/09 |
|
NASA Dryden's Starr Ginn: En
Read News Feature NASA Dryde
3/25/09
Description |
Read News Feature NASA Dryden engineer Starr Ginn shows off components of an aircraft jacking system that allows an aircraft to "float" during testing or maintenance. Ginn designed, assembled, and tested this hardware that is now in use for several of Dryden's aircraft. March 19, 2009 NASA Photo / Tom Tschida ED09-0067-2 |
Date |
3/25/09 |
|
Photo Description |
NASA's Hyper-X Program Manager Vince Rausch talks about the X-43 [ http://www.dfrc.nasa.gov/Gallery/Photo/X-43A/index.html ] from his office at NASA Langley Research Center in Hampton, VA. |
Project Description |
Vincent L. Rausch was named Hyper-X Program Manager and started working at NASA Langley Research Center in July 1996. He is responsible for the overall execution of the joint Langley ? NASA Dryden Flight Research Center Hyper-X program which will flight-validate the performance of an airframe-integrated supersonic combustion ramjet (scramjet) engine installed on an X-43 research aircraft [ http://www.dfrc.nasa.gov/Gallery/Photo/X-43A/index.html ]. Mr. Rausch joined the NASA Headquarters Office of Aeronautics in 1991 as the Assistant Director for Aeronautics (High-Performance Aircraft). In this capacity, he coordinated NASA high-performance aircraft programs with the Department of Defense. In 1992, he was appointed Director for National Aero-Space Plane (NASP) and served as the agency focal point for NASA involvement in the DOD ? NASA NASP program. In 1995, as Director, Inter-Enterprise Operations, he coordinated Aeronautics Enterprise activities with the other NASA enterprises (Space Science, Earth Science, and Human Exploration and Development of Space). Before retiring as a colonel from the U.S. Air Force in 1991, Mr. Rausch spent three years as the first Director of the NASP Inter-Agency Office (NIO) in the Pentagon. His NIO responsibilities included the DOD portion of the NASP budget, congressional liaison, and day-to-day coordination with NASA. From 1986 to 1988, he served in the NASP Joint Program Office (JPO) at Wright-Patterson AFB, OH. His positions included acting Program Manager, Director of Program Operations, and Director of Systems Applications. From 1982 to 1986, while assigned to the Aeronautical Systems Division (ASD), at Wright-Patterson AFB, he directed the Transatmospheric Vehicle (TAV) program which examined single- and two-stage-to-orbit military spaceplanes. He also led ASD participation in the Copper Canyon program, the Defense Advanced Research Projects Agency-funded effort which established the feasibility of the NASP. His Strategic Air Command operational experience includes over 3,000 hours in the B-52 and 56 combat missions. Mr. Rausch is the recipient of the Air Force Legion of Merit, Defense Meritorious Service Medal, Air Force Meritorious Service Medal, Air Medal (with two oak leaf clusters), Air Force Commendation Medal (with one oak leaf cluster) and a NASA Outstanding Service Award. He has a BA from Coe College, Cedar Rapids, IA, and an MBA from Inter-American University, San Germain, PR. He is also a graduate of the Federal Executive Institute, Air War College, Armed Forces Staff College, Air Command and Staff College, and Squadron Officer School. A native of Charlottesville, VA, Mr. Rausch and his wife, Diane, reside in Williamsburg, Virginia. |
Photo Date |
February 11, 2004 |
|
Photo Description |
NASA personnel in a control room during the successful second flight of the X-43A aircraft. front row, left to right: Randy Voland, LaRC Propulsion, Craig Christy, Boeing Systems, Dave Reubush, NASA Hyper-X Deputy Program Manager, and Vince Rausch, NASA Hyper-X Program Manager. back row, left to right: Bill Talley, DCI/consultant, Pat Stoliker, DFRC Director (Acting) of Research Engineering, John Martin, LaRC G&C, and Dave Bose, AMA/Controls. |
Project Description |
The high-risk, high-payoff X-43A flights are the first actual flight tests of an aircraft powered by a scramjet engine capable of operating at hypersonic speeds (above Mach 5, or five times the speed of sound). The X-43A is powered by a revolutionary air-breathing supersonic-combustion ramjet or "scramjet" engine. In a combined research effort involving Dryden, Langley, and several industry partners, NASA demonstrated the value of its X-43A hypersonic research aircraft, as it became the first air-breathing, unpiloted, scramjet-powered plane to fly freely by itself. The March 27 flight, originating from NASA's Dryden Flight Research Center, began with the Agency's B-52B launch aircraft carrying the X-43A out to the test range over the Pacific Ocean off the California coast. The X-43A was boosted up to its test altitude of about 95,000 feet, where it separated from its modified Pegasus booster and flew freely under its own power. Two very significant aviation milestones occurred during this test flight: first, controlled accelerating flight at Mach 7 under scramjet power, and second, the successful stage separation at high dynamic pressure of two non-axisymmetric vehicles. To top it all off, the flight resulted in the setting of a new aeronautical speed record. The X-43A reached a speed of over Mach 7, or about 5,000 miles per hour faster than any known aircraft powered by an air-breathing engine has ever flown. |
Photo Date |
March 27, 2004 |
|
Photo Description |
F-8 DFBW in flight |
Project Description |
The F-8 Digital Fly-By-Wire (DFBW) flight research project validated the principal concepts of all-electric flight control systems now used on nearly all modern high-performance aircraft and on military and civilian transports. The first flight of the 13-year project was on May 25, 1972, with research pilot Gary E. Krier at the controls of a modified F-8C Crusader that served as the testbed for the fly-by-wire technologies. The project was a joint effort between the NASA Flight Research Center, Edwards, California, (now the Dryden Flight Research Center) and Langley Research Center. It included a total of 211 flights. The last flight was December 16, 1985, with Dryden research pilot Ed Schneider at the controls. The F-8 DFBW system was the forerunner of current fly-by-wire systems used in the space shuttles and on today?s military and civil aircraft to make them safer, more maneuverable, and more efficient. Electronic fly-by-wire systems replaced older hydraulic control systems, freeing designers to design aircraft with reduced in-flight stability. Fly-by-wire systems are safer because of their redundancies. They are more maneuverable because computers can command more frequent adjustments than a human pilot can. For airliners, computerized control ensures a smoother ride than a human pilot alone can provide. Digital-fly-by-wire is more efficient because it is lighter and takes up less space than the hydraulic systems it replaced. This either reduces the fuel required to fly or increases the number of passengers or pounds of cargo the aircraft can carry. Digital fly-by-wire is used in a variety of aircraft ranging from F/A-18 fighters to the Boeing 777. The DFBW research program is considered one of the most significant and most successful NASA aeronautical programs since the inception of the agency. F-8 aircraft were built originally for the U.S. Navy by LTV Aerospace of Dallas, Texas. The aircraft had a wingspan of 35 feet, 2 inches, was 54 feet, 6 inches long, and was powered by a Pratt & Whitney J57 turbojet engine. |
Photo Date |
January 10, 1973 |
|
M2-F1 and M2-F2 lifting bodi
Project Description |
The wingless, lifting body aircraft design was initially conceived as a means of landing an aircraft horizontally after atmospheric reentry. The absence of wings would make the extreme heat of re-entry less damaging to the vehicle. In 1962, Dryden management approved a program to build a lightweight, unpowered lifting body as a prototype to flight test the wingless concept. It would look like a "flying bathtub," and was designated the M2-F1, the "M" referring to "manned" and "F" referring to "flight" version. It featured a plywood shell placed over a tubular steel frame crafted at Dryden. Construction was completed in 1963. The first flight tests of the M2-F1 were over Rogers Dry Lake at the end of a tow rope attached to a hopped-up Pontiac convertible driven at speeds up to about 120 mph. This vehicle needed to be able to tow the M2-F1 on the Rogers Dry Lakebed adjacent to NASA's Flight Research Center (FRC) at a minimum speed of 100 miles per hour. To do that, it had to handle the 400-pound pull of the M2-F1. Walter "Whitey" Whiteside, who was a retired Air Force maintenance officer working in the FRC's Flight Operations Division, was a dirt-bike rider and hot-rodder. Together with Boyden "Bud" Bearce in the Procurement and Supply Branch of the FRC, Whitey acquired a Pontiac Catalina convertible with the largest engine available. He took the car to Bill Straup's renowned hot-rod shop near Long Beach for modification. With a special gearbox and racing slicks, the Pontiac could tow the 1,000-pound M2-F1 110 miles per hour in 30 seconds. It proved adequate for the roughly 400 car tows that got the M2-F1 airborne to prove it could fly safely and to train pilots before they were towed behind a C-47 aircraft and released. These initial car-tow tests produced enough flight data about the M2-F1 to proceed with flights behind the C-47 tow plane at greater altitudes. The C-47 took the craft to an altitude of 12,000 where free flights back to Rogers Dry Lake began. Pilot for the first series of flights of the M2-F1 was NASA research pilot Milt Thompson. Typical glide flights with the M2-F1 lasted about two minutes and reached speeds of 110 to 120 mph. A small solid landing rocket, referred to as the "instant L/D rocket," was installed in the rear base of the M2-F1. This rocket, which could be ignited by the pilot, provided about 250 pounds of thrust for about 10 seconds. The rocket could be used to extend the flight time near landing if needed. More than 400 ground tows and 77 aircraft tow flights were carried out with the M2-F1. The success of Dryden's M2-F1 program led to NASA's development and construction of two heavyweight lifting bodies based on studies at NASA's Ames and Langley research centers--the M2-F2 and the HL-10, both built by the Northrop Corporation, and the U.S. Air Force's X-24 program, with an X-24A and -B built by Martin. The Lifting Body program also heavily influenced the Space Shuttle program. The M2-F1 program demonstrated, the feasibility of the lifting body concept for horizontal landings of atmospheric entry vehicles. It also demonstrated a procurement and management concept for prototype flight test vehicles that produced rapid results at very low cost (approximately $50,000, excluding salaries of government employees assigned to the project). A fleet of lifting bodies flown at the NASA Dryden Flight Research Center, Edwards, California, from 1963 to 1975 demonstrated the ability of pilots to maneuver and safely land a wingless vehicle designed to fly back to Earth from space and be landed like an aircraft at a pre-determined site. Aerodynamic lift--essential to flight in the atmosphere--was obtained from the shape of their bodies. The addition of fins and control surfaces allowed the pilots to stabilize and control the vehicles and regulate their flight paths. The information the lifting body program generated contributed to the data base that led to development of today's space shuttle program. The success of Dryden's M2-F1 [ http://www.dfrc.nasa.gov/Gallery/Photo/M2-F1/index.html ] program led to NASA's development and construction of two heavyweight lifting bodies based on studies at NASA's Ames and Langley research centers--the M2-F2 and the HL-10, both built by the Northrop Corporation. The "M" refers to "manned" and "F" refers to "flight" version. "HL" comes from "horizontal landing" and 10 is for the tenth lifting body model to be investigated by Langley. The first flight of the M2-F2--which looked much like the "F1"--was on July 12, 1966. Milt Thompson was the pilot. By then, the same B-52s used to air launch the famed X-15 rocket research aircraft were modified to also carry the lifting bodies. Thompson was dropped from the B-52's wing pylon mount at an altitude of 45,000 feet on that maiden glide flight. The M2-F2 weighed 4,620 pounds, was 22 feet long, and had a width of about 10 feet. On May 10, 1967, during the sixteenth glide flight leading up to powered flight, a landing accident severely damaged the vehicle and seriously injured the NASA pilot, Bruce Peterson. NASA pilots and researchers realized the M2-F2 had lateral control problems, even though it had a stability augmentation (control) system. When the M2-F2 was rebuilt at Dryden and redesignated the M2-F3 [ http://www.dfrc.nasa.gov/Gallery/Photo/M2-F3/index.html ], it was modified with an additional third vertical fin--centered between the tip fins--to improve control characteristics. The M2-F2/F3 was the first of the heavy-weight, entry-configuration (i.e., configured for re-entry to the atmosphere from space) lifting bodies. Its successful development as a research test vehicle answered many of the generic questions about these vehicles. NASA donated the M2-F3 vehicle to the Smithsonian Institute in December 1973. It is currently hanging in the Air and Space Museum along with the X-15 aircraft number 1, which was its hangar partner at Dryden from 1965 to 1969. |
Photo Date |
February 24, 1966 |
|
CERES Ocean Validation Exper
At the mouth of the Chesapea
8/13/09
Description |
At the mouth of the Chesapeake Bay is a unique instrument platform: the Coast Guard's Chesapeake Lighthouse. Taking advantage of it's open ocean location far from typical land-based factors, Science Directorate researchers use the lighthouse to maintain a suite of instruments that provide continuous radiation measurements and validate or provide ground truth for the satellite-based CERES instruments. Collectively, the suite of instruments is called the CERES Ocean Validation Experiment (COVE). Clouds and the Earth's Radiant Energy System -- or CERES -- data provide key knowledge about Earth's changing climate and are used to study the energy exchanged between the Sun, the Earth's atmosphere, surface and clouds, and space. COVE instruments and measurements include the Baseline Surface Radiation Network instrument suite -- uplooking shaded and unshaded broadband pyranometers, shaded pyrgeometers, downlooking pyranometers and pyrgeometers, normal incidence pyrheliometers, an AERONET sunphotometer, uplooking and downlooking multifilter rotating shadowband radiometers (MFRSRs), a micropulse lidar, pressure, temperature, relative humidity, National Oceanic and Atmospheric Administration (NOAA) global positioning system integrated precipitable water vapor (GPS-IPW), and National Data Buoy Center (NDBC) wave height and period. Fred Denn, a COVE scientist with SSAI at NASA Langley, adjusts an instrument on the lookout tower of the lighthouse, about 120 feet (36.5 m) above the ocean surface. Langley researchers travel to the lighthouse every few weeks to adjust and maintain the instruments and conduct research. Credit: NASA/Sean Smith |
Date |
8/13/09 |
|
First B-52 captive flight of
X-43A / Hyper-X separation f
X-43A / Hyper-X / Pegasus st
Pegasus Mated under Wing of
Photo Description |
A close-up view of the Pegasus space-booster attached to the wing pylon of NASA?s B-52 launch aircraft at NASA's Dryden Flight Research Center, Edwards, California. The Pegasus rocket booster was designed as a way to get small payloads into space orbit more easily and cost-effectively. It has also been used to gather data on hypersonic flight. |
Project Description |
Pegasus is an air-launched space booster produced by Orbital Sciences Corporation and Hercules Aerospace Company (initially, later, Alliant Tech Systems) to provide small satellite users with a cost-effective, flexible, and reliable method for placing payloads into low earth orbit. Pegasus has been used to launch a number of satellites and the PHYSX experiment. That experiment consisted of a smooth glove installed on the first-stage delta wing of the Pegasus. The glove was used to gather data at speeds of up to Mach 8 and at altitudes approaching 200,000 feet. The flight took place on October 22, 1998. The PHYSX experiment focused on determining where boundary-layer transition occurs on the glove and on identifying the flow mechanism causing transition over the glove. Data from this flight-research effort included temperature, heat transfer, pressure measurements, airflow, and trajectory reconstruction. Hypersonic flight-research programs are an approach to validate design methods for hypersonic vehicles (those that fly more than five times the speed of sound, or Mach 5). Dryden Flight Research Center, Edwards, California, provided overall management of the glove experiment, glove design, and buildup. Dryden also was responsible for conducting the flight tests. Langley Research Center, Hampton, Virginia, was responsible for the design of the aerodynamic glove as well as development of sensor and instrumentation systems for the glove. Other participating NASA centers included Ames Research Center, Mountain View, California, Goddard Space Flight Center, Greenbelt, Maryland, and Kennedy Space Center, Florida. Orbital Sciences Corporation, Dulles, Virginia, is the manufacturer of the Pegasus vehicle, while Vandenberg Air Force Base served as a pre-launch assembly facility for the launch that included the PHYSX experiment. NASA used data from Pegasus launches to obtain considerable data on aerodynamics. By conducting experiments in a piggyback mode on Pegasus, some critical and secondary design and development issues were addressed at hypersonic speeds. The vehicle was also used to develop hypersonic flight instrumentation and test techniques. NASA's B-52 carrier-launch vehicle was used to get the Pegasus airborne during six launches from 1990 to 1994. Thereafter, an Orbital Sciences L-1011 aircraft launched the Pegasus. The Pegasus launch vehicle itself has a 400- to 600-pound payload capacity in a 61-cubic-foot payload space at the front of the vehicle. The vehicle is capable of placing a payload into low earth orbit. This vehicle is 49 feet long and 50 inches in diameter. It has a wing span of 22 feet. (There is also a Pegasus XL vehicle that was introduced in 1994. Dryden has never launched one of these vehicles, but they have greater thrust and are 56 feet long.) |
Photo Date |
August 2, 1994 |
|
PHYSX Glove Test
Photo Description |
A mock-up of the stainless-steel Pegasus Hypersonic Experiment (PHYSX) Projects experimental "glove" undergoes hot-loads tests at NASA's Dryden Flight Research Center, Edwards, California. The thermal ground test simulates heats and pressures the wing glove will experience at hypersonic speeds. Quartz heat lamps subject this model of a Pegasus booster rocket's right wing glove to the extreme heats it will experience at speeds approaching Mach 8. The glove has a highly reflective surface, underneath which are hundreds of temperature and pressure sensors that will send hypersonic flight data to ground tracking facilities during the experimental flight. |
Project Description |
Pegasus is an air-launched space booster produced by Orbital Sciences Corporation and Hercules Aerospace Company (initially, later, Alliant Tech Systems) to provide small satellite users with a cost-effective, flexible, and reliable method for placing payloads into low earth orbit. Pegasus has been used to launch a number of satellites and the PHYSX experiment. That experiment consisted of a smooth glove installed on the first-stage delta wing of the Pegasus. The glove was used to gather data at speeds of up to Mach 8 and at altitudes approaching 200,000 feet. The flight took place on October 22, 1998. The PHYSX experiment focused on determining where boundary-layer transition occurs on the glove and on identifying the flow mechanism causing transition over the glove. Data from this flight-research effort included temperature, heat transfer, pressure measurements, airflow, and trajectory reconstruction. Hypersonic flight-research programs are an approach to validate design methods for hypersonic vehicles (those that fly more than five times the speed of sound, or Mach 5). Dryden Flight Research Center, Edwards, California, provided overall management of the glove experiment, glove design, and buildup. Dryden also was responsible for conducting the flight tests. Langley Research Center, Hampton, Virginia, was responsible for the design of the aerodynamic glove as well as development of sensor and instrumentation systems for the glove. Other participating NASA centers included Ames Research Center, Mountain View, California, Goddard Space Flight Center, Greenbelt, Maryland, and Kennedy Space Center, Florida. Orbital Sciences Corporation, Dulles, Virginia, is the manufacturer of the Pegasus vehicle, while Vandenberg Air Force Base served as a pre-launch assembly facility for the launch that included the PHYSX experiment. NASA used data from Pegasus launches to obtain considerable data on aerodynamics. By conducting experiments in a piggyback mode on Pegasus, some critical and secondary design and development issues were addressed at hypersonic speeds. The vehicle was also used to develop hypersonic flight instrumentation and test techniques. NASA's B-52 carrier-launch vehicle was used to get the Pegasus airborne during six launches from 1990 to 1994. Thereafter, an Orbital Sciences L-1011 aircraft launched the Pegasus. The Pegasus launch vehicle itself has a 400- to 600-pound payload capacity in a 61-cubic-foot payload space at the front of the vehicle. The vehicle is capable of placing a payload into low earth orbit. This vehicle is 49 feet long and 50 inches in diameter. It has a wing span of 22 feet. (There is also a Pegasus XL vehicle that was introduced in 1994. Dryden has never launched one of these vehicles, but they have greater thrust and are 56 feet long.) |
Photo Date |
September 13, 1995 |
|
NASA Presents Safety Award t
Read News Release 09-07 NASA
2/25/09
Description |
Read News Release 09-07 NASA has presented its Quality and Safety Achievement Recognition, or QASAR, award for 2008 to Daniel J. Crowley, director of Facilities Engineering and Asset Management at NASA's Dryden Flight Research Center. Photo Description: Daniel J. Crowley Director, Facilities Engineering and Asset Management NASA Dryden Flight Research Center NASA Photo ED07-0150-09 |
Date |
2/25/09 |
|
Chief pilot Gordon Fullerton
NASA Dryden Flight Research
9/30/08
Description |
NASA Dryden Flight Research Center's chief pilot Gordon Fullerton in the cockpit of the center's T-38 Talon mission support aircraft. February 24, 2005 NASA / Photo Tony Landis EC05-0041-5 |
Date |
9/30/08 |
|
Shuttle Columbia in the Mate
The Space Shuttle Columbia c
10/9/08
Description |
The Space Shuttle Columbia can be seen in the post-flight processing facility known as the MDD (Mate-Demate Device) at NASA's Dryden Flight Research Center, CA, in this aerial view taken shortly after completing its first orbital mission with a landing at Edwards Air Force Base. April, 1981 NASA / Photo ECN-14962 |
Date |
10/9/08 |
|
Dryden technician Robert Fle
ED09-0183-16 NASA's Dryden F
8/7/09
Description |
ED09-0183-16 NASA's Dryden Flight Research Center recently conducted a flight test of an airflow-measurement device mounted underneath its F-15B research aircraft in the Rake Airflow Gage Experiment, or RAGE. July 14, 2009 NASA photo / Tony Landis |
Date |
8/7/09 |
|
Ikhana Resumes Fire Mission
NASA's Autonomous Modular Sc
9/22/08
Description |
NASA's Autonomous Modular Scanner mounted on the Ikhana remotely piloted aircraft captured this thermal-infrared imagery during two passes over the Hidden wildfire during a flight over the southern Sierras about 30 miles northeast of Visalia in Central California on Sept. 19, 2008. This false-color, three-dimensional image shows unburned vegetation in green, smoke and bare areas in bluish-white and fire hot spots in yellow and red, overlaid on a Google Earth Digital Globe terrain image. Text credit: NASA's Dryden Flight Research Center > Read more about the Ikhana mission |
Date |
9/22/08 |
|
Dryden F-8 Research Aircraft
Photo Description |
F-8 Digital Fly-By-Wire (left) and F-8 Supercritical Wing in flight. These two aircraft fundamentally changed the nature of aircraft design. The F-8 DFBW pioneered digital flight controls and led to such computer-controlled aircraft as the F-117A, X-29, and X-31. Airliners such as the Boeing 777 and Airbus A320 also use digital fly-by-wire systems. The other aircraft is a highly modified F-8A fitted with a supercritical wing. Dr. Richard T. Whitcomb of Langley Research Center originated the supercritical wing concept in the late 1960s. (Dr. Whitcomb also developed the concept of the "area rule" in the early 1950s. It significantly reduced transonic drag.) |
Project Description |
The F-8 Digital Fly-By-Wire (DFBW) flight research project validated the principal concepts of all-electric flight control systems now used on nearly all modern high-performance aircraft and on military and civilian transports. The first flight of the 13-year project was on May 25, 1972, with research pilot Gary E. Krier at the controls of a modified F-8C Crusader that served as the testbed for the fly-by-wire technologies. The project was a joint effort between the NASA Flight Research Center, Edwards, California, (now the Dryden Flight Research Center) and Langley Research Center. It included a total of 211 flights. The last flight was December 16, 1985, with Dryden research pilot Ed Schneider at the controls. The F-8 DFBW system was the forerunner of current fly-by-wire systems used in the space shuttles and on today's military and civil aircraft to make them safer, more maneuverable, and more efficient. Electronic fly-by-wire systems replaced older hydraulic control systems, freeing designers to design aircraft with reduced in-flight stability. Fly-by-wire systems are safer because of their redundancies. They are more maneuverable because computers can command more frequent adjustments than a human pilot can. For airliners, computerized control ensures a smoother ride than a human pilot alone can provide. Digital-fly-by-wire is more efficient because it is lighter and takes up less space than the hydraulic systems it replaced. This either reduces the fuel required to fly or increases the number of passengers or pounds of cargo the aircraft can carry. Digital fly-by-wire is currently used in a variety of aircraft ranging from F/A-18 fighters to the Boeing 777. The DFBW research program is considered one of the most significant and most successful NASA aeronautical programs since the inception of the agency. F-8 aircraft were built originally for the U.S. Navy by LTV Aerospace of Dallas, Texas. The aircraft had a wingspan of 35 feet, 2 inches, was 54 feet, 6 inches long, and was powered by a Pratt & Whitney J57 turbojet engine. The F-8 Supercritical Wing was a flight research project designed to test a new wing concept designed by Dr. Richard Whitcomb, chief of the Transonic Aerodynamics Branch, Langley Research Center, Hampton, Virginia. Compared to a conventional wing, the supercritical wing (SCW) is flatter on the top and rounder on the bottom with a downward curve at the trailing edge. The Supercritical Wing was designed to delay the formation of and reduce the shock wave over the wing just below and above the speed of sound (transonic region of flight). Delaying the shock wave at these speeds results in less drag. Results of the NASA flight research at the Flight Research Center, Edwards, California, (later renamed the Dryden Flight Research Center) demonstrated that aircraft using the supercritical wing concept would have increased cruising speed, improved fuel efficiency, and greater flight range than those using conventional, wings. As a result, supercritical wings are now commonplace on virtually every modern subsonic commercial transport. Results of the NASA project showed the SCW had increased the transonic efficiency of the F-8 as much as 15 percent and proved that passenger transports with supercritical wings, versus conventional wings, could save $78 million (in 1974 dollars) per year for a fleet of 280 200-passenger airliners. The F-8 Supercritical Wing (SCW) project flew from 1970 to 1973. Dryden engineer John McTigue was the first SCW program manager and Tom McMurtry was the lead project pilot. The first SCW flight took place on March 9, 1971. The last flight of the Supercritical wing was on May 23, 1973, with Ron Gerdes at the controls. Original wingspan of the F-8 is 35 feet, 2 inches while the wingspan with the supercritical wing was 43 feet, 1 inch. F-8 aircraft were powered by Pratt & Whitney J57 turbojet engines. The TF-8A Crusader was made available to the NASA Flight Research Center by the U.S. Navy. F-8 jet aircraft were built, originally, by LTV Aerospace, Dallas, Texas. Rockwell International's North American Aircraft Division received a $1.8 million contract to fabricate the supercritical wing, which was delivered to NASA in December 1969. |
Photo Date |
January 10, 1973 |
|
M2-F3 with test pilot John A
Photo Description |
NASA research pilot John A. Manke is seen here in front of the M2-F3 Lifting Body. Manke was hired by NASA on May 25, 1962, as a flight research engineer. He was later assigned to the pilot's office and flew various support aircraft including the F-104, F5D, F-111 and C-47. After leaving the Marine Corps in 1960, Manke worked for Honeywell Corporation as a test engineer for two years before coming to NASA. He was project pilot on the X-24B and also flew the HL-10, M2-F3, and X-24A lifting bodies. John made the first supersonic flight of a lifting body and the first landing of a lifting body on a hard surface runway. Manke served as Director of the Flight Operations and Support Directorate at the Dryden Flight Research Center prior to its integration with Ames Research Center in October 1981. After this date John was named to head the joint Ames-Dryden Directorate of Flight Operations. He also served as site manager of the NASA Ames-Dryden Flight Research Facility. John is a member of the Society of Experimental Test Pilots. He retired on April 27, 1984. |
Project Description |
A fleet of lifting bodies flown at the NASA Flight Research Center (FRC--later the Dryden Flight Research Center), Edwards, California, from 1963 to 1975 demonstrated the ability of pilots to maneuver and safely land a wingless vehicle designed to fly back to Earth from space and be landed like an aircraft at a pre-determined site. Aerodynamic lift--essential to flight in the atmosphere--was obtained from the shape of their bodies. The addition of fins and control surfaces allowed the pilots to stabilize and control the vehicles and regulate their flight paths. The information the lifting body program generated contributed to the data base that led to development of today's space shuttle program. The success of the FRC's M2-F1 [ http://www.dfrc.nasa.gov/Gallery/Photo/M2-F1/index.html ] program led to NASA's development and construction of two heavyweight lifting bodies based on studies at NASA's Ames and Langley research centers--the M2-F2 and the HL-10, both built by the Northrop Corporation. The "M" refers to "manned" and "F" refers to "flight" version. "HL" comes from "horizontal landing" and 10 is for the tenth lifting body model to be investigated by Langley. The first flight of the M2-F2--which looked much like the "F1"--was on July 12, 1966. Milt Thompson was the pilot. By then, the same B-52s used to air launch the famed X-15 rocket research aircraft were modified to also carry the lifting bodies. Thompson was dropped from the B-52's wing pylon mount at an altitude of 45,000 feet on that maiden glide flight. The M2-F2 weighed 4,620 pounds, was 22 feet long, and had a width of about 10 feet. On May 10, 1967, during the sixteenth glide flight leading up to powered flight, a landing accident severely damaged the vehicle and seriously injured the NASA pilot, Bruce Peterson. NASA pilots and researchers realized the M2-F2 had lateral control problems, even though it had a stability augmentation (control) system. When the M2-F2 was rebuilt by the Northrop Corporation with the help and cooperation of the FRC and redesignated the M2-F3 [ http://www.dfrc.nasa.gov/Gallery/Photo/M2-F3/index.html ], it was modified with an additional third vertical fin--centered between the tip fins--to improve control characteristics. The M2-F2/F3 was the first of the heavy-weight, entry-configuration (i.e., configured for re-entry to the atmosphere from space) lifting bodies. Its successful development as a research test vehicle answered many of the generic questions about these vehicles. NASA donated the M2-F3 vehicle to the Smithsonian Institute in December 1973. It is currently hanging in the Air and Space Museum along with the X-15 aircraft number 1, which was its hangar partner at Dryden from 1965 to 1969. |
Photo Date |
December 20, 1972 |
|
F-8 SCW on ramp with test pi
Photo Description |
A Vought F-8A Crusader was selected by NASA as the testbed aircraft (designated TF-8A) to install an experimental Supercritical Wing (SCW) in place of the conventional wing. The unique design of the Supercritical Wing reduces the effect of shock waves on the upper surface near Mach 1, which in turn reduces drag. In this photograph the TF-8A Crusader with Supercritical Wing is shown on the ramp with project pilot Tom McMurtry standing beside it. McMurtry received NASA's Exceptional Service Medal for his work on the F-8 SCW aircraft. He also flew the AD-1, F-15 Digital Electronic Engine Control, the KC-130 winglets, the F-8 Digital Fly-By-Wire and other flight research aircraft including the remotely piloted 720 Controlled Impact Demonstration and sub-scale F-15 research projects. In addition, McMurtry was the 747 co-pilot for the Shuttle Approach and Landing Tests and made the last glide flight in the X-24B. McMurtry was Dryden?s Director for Flight Operations from 1986 to 1998, when he became Associate Director for Operations at NASA Dryden. In 1982, McMurtry received the Iven C. Kincheloe Award from the Society of Experimental Test Pilots for his contributions as project pilot on the AD-1 Oblique Wing program. In 1998 he was named as one of the honorees at the Lancaster, Calif., ninth Aerospace Walk of Honor ceremonies. In 1999 he was awarded the NASA Distinguished Service Medal. He retired in 1999 after a distinguished career as pilot and manager at Dryden that began in 1967. |
Project Description |
The F-8 Supercritical Wing was a flight research project designed to test a new wing concept designed by Dr. Richard Whitcomb, chief of the Transonic Aerodynamics Branch, Langley Research Center, Hampton, Virginia. Compared to a conventional wing, the supercritical wing (SCW) is flatter on the top and rounder on the bottom with a downward curve at the trailing edge. The Supercritical Wing was designed to delay the formation of and reduce the shock wave over the wing just below and above the speed of sound (transonic region of flight). Delaying the shock wave at these speeds results in less drag. Results of the NASA flight research at the Flight Research Center, Edwards, California, (later renamed the Dryden Flight Research Center) demonstrated that aircraft using the supercritical wing concept would have increased cruising speed, improved fuel efficiency, and greater flight range than those using conventional wings. As a result, supercritical wings are now commonplace on virtually every modern subsonic commercial transport. Results of the NASA project showed the SCW had increased the transonic efficiency of the F-8 as much as 15 percent and proved that passenger transports with supercritical wings, versus conventional wings, could save $78 million (in 1974 dollars) per year for a fleet of 280 200-passenger airliners. The F-8 Supercritical Wing (SCW) project flew from 1970 to 1973. Dryden engineer John McTigue was the first SCW program manager and Tom McMurtry was the lead project pilot. The first SCW flight took place on March 9, 1971. The last flight of the Supercritical wing was on May 23, 1973, with Ron Gerdes at the controls. Original wingspan of the F-8 is 35 feet, 2 inches while the wingspan with the supercritical wing was 43 feet, 1 inch. F-8 aircraft were powered by Pratt & Whitney J57 turbojet engines. The TF-8A Crusader was made available to the NASA Flight Research Center by the U.S. Navy. F-8 jet aircraft were built, originally, by LTV Aerospace, Dallas, Texas. Rockwell International?s North American Aircraft Division received a $1.8 million contract to fabricate the supercritical wing, which was delivered to NASA in December 1969. |
Photo Date |
December 20, 1972 |
|
Dryden Engine Shop
F404-400 jet engines. Januar
2/12/09
Description |
F404-400 jet engines. January 29, 2009 NASA Photo / Tony Landis ED09-0019-42 |
Date |
2/12/09 |
|
M2-F1 in flight being towed
Photo Description |
The M2-F1 Lifting Body is seen here being towed behind a C-47 at the Flight Research Center (later redesignated the Dryden Flight Research Center), Edwards, California. In this rear view, the M2-F1 is flying above and to one side of the C-47. This was done to avoid wake turbulence from the towplane. Lacking wings, the M2-F1 used an unusual configuration for its control surfaces. It had two rudders on the fins, two elevons (called "elephant ears") mounted on the outsides of the fins, and two body flaps on the upper rear fuselage. |
Project Description |
The wingless, lifting body aircraft design was initially conceived as a means of landing an aircraft horizontally after atmospheric reentry. The absence of wings would make the extreme heat of re-entry less damaging to the vehicle. In 1962, Dryden management approved a program to build a lightweight, unpowered lifting body as a prototype to flight test the wingless concept. It would look like a "flying bathtub," and was designated the M2-F1, the "M" referring to "manned" and "F" referring to "flight" version. It featured a plywood shell placed over a tubular steel frame crafted at Dryden. Construction was completed in 1963. The first flight tests of the M2-F1 were over Rogers Dry Lake at the end of a tow rope attached to a hopped-up Pontiac convertible driven at speeds up to about 120 mph. These initial tests produced enough flight data about the M2-F1 to proceed with flights behind the C-47 tow plane at greater altitudes. The C-47 took the craft to an altitude of 12,000 where free flights back to Rogers Dry Lake began. Pilot for the first series of flights of the M2-F1 was NASA research pilot Milt Thompson. Typical glide flights with the M2-F1 lasted about two minutes and reached speeds of 110 to 120 mph. More than 400 ground tows and 77 aircraft tow flights were carried out with the M2-F1. The success of Dryden's M2-F1 program led to NASA's development and construction of two heavyweight lifting bodies based on studies at NASA's Ames and Langley research centers--the M2-F2 and the HL-10, both built by the Northrop Corporation, and the U.S. Air Force's X-24 program. The Lifting Body program also heavily influenced the Space Shuttle program. The M2-F1 program demonstrated the feasibility of the lifting body concept for horizontal landings of atmospheric entry vehicles. It also demonstrated a procurement and management concept for prototype flight test vehicles that produced rapid results at very low cost (approximately $50,000, excluding salaries of government employees assigned to the project). |
Photo Date |
February 28, 1964 |
|
M2-F1 ground test firing of
Photo Description |
The M2-F1 Lifting Body is seen here testing its "instant L/D rocket" on the lakebed at NASA's Flight Research Center (later redesignated the Dryden Flight Research Center), Edwards, California. The M2-F1 was an experimental aircraft. Its outer plywood shell was built by sailplane maker Gus Briegleb, while the internal frame was built at the Flight Research Center. The instant lift-over-drag (L/D) rocket was developed at the Navy facility at China Lake, California |
Project Description |
The wingless, lifting body aircraft design was initially concieved as a means of landing an aircraft horizontally after atmospheric reentry. The absence of wings would make the extreme heat of re-entry less damaging to the vehicle. In 1962, Dryden management approved a program to build a lightweight, unpowered lifting body as a prototype to flight test the wingless concept. It would look like a "flying bathtub," and was designated the M2-F1, the "M" referring to "manned" and "F" referring to "flight" version. It featured a plywood shell placed over a tubular steel frame crafted at Dryden. Construction was completed in 1963. The first flight tests of the M2-F1 were over Rogers Dry Lake at the end of a tow rope attached to a hopped-up Pontiac convertible driven at speeds up to about 120 mph. These initial tests produced enough flight data about the M2-F1 to proceed with flights behind the C-47 tow plane at greater altitudes. The C-47 took the craft to an altitude of 12,000 where free flights back to Rogers Dry Lake began. Pilot for the first series of flights of the M2-F1 was NASA research pilot Milt Thompson. Typical glide flights with the M2-F1 lasted about two minutes and reached speeds of 110 to l20 mph. A small solid landing rocket, referred to as the "instant L/D rocket," was installed in the rear base of the M2-F1. This rocket, which could be ignited by the pilot, provided about 250 pounds of thrust for about 10 seconds. The rocket could be used to extend the flight time near landing if needed. More than 400 ground tows and 77 aircraft tow flights were carried out with the M2-F1. The success of Dryden's M2-F1 program led to NASA's development and construction of two heavyweight lifting bodies based on studies at NASA's Ames and Langley research centers--the M2-F2 and the HL-10, both built by the Northrop Corporation, and the U.S. Air Force's X-24 program, with an X-24A and -B built by Martin. The Lifting Body program also heavily influenced the Space Shuttle program. The M2-F1 program demonstrated the feasibility of the lifting body concept for horizontal landings of atmospheric entry vehicles. It also demonstrated a procurement and management concept for prototype flight test vehicles that produced rapid results at very low cost (approximately $50,000, excluding salaries of government employees assigned to the project). |
Photo Date |
August 5, 1963 |
|
Dryden's two T-38A Mission S
NASA Dryden's two T-38A miss
10/6/08
Description |
NASA Dryden's two T-38A mission support aircraft fly in tight formation while conducting a pitot-static airspeed calibration check near Edwards Air Force Base. September 26, 2007 NASA / Photo Jim Ross ED07-0222-06 |
Date |
10/6/08 |
|
NASA Dryden's Starr Ginn: En
Read News Feature NASA Dryde
3/25/09
Description |
Read News Feature NASA Dryden engineer Starr Ginn works with Catlin Level, Summer High School Apprenticeship Research Program intern, to assemble an aircraft jacking system she designed that allows an aircraft to "float" during testing or maintenance. July 19, 2004 NASA photo / Tom Tschida EC04-0215-4 |
Date |
3/25/09 |
|
Dryden's T-34C on Mission Su
Chase aircraft such as the T
10/10/08
Description |
Chase aircraft such as the T-34C accompany research flights for photography and video purposes. They also provide support for safety and research. At Dryden, the T-34 is used mainly for smaller remotely piloted vehicles which fly slower than NASA's F-18's, used for larger scale projects. June 20, 2005 NASA / Photo Jim Ross EC05-0133-01 |
Date |
10/10/08 |
|
Beech T-34C is Flown by NASA
Chase aircraft such as the T
10/10/08
Description |
Chase aircraft such as the T-34C accompany research flights for photography and video purposes. They also provide support for safety and research. At Dryden, the T-34 is used mainly for smaller remotely piloted vehicles which fly slower than NASA's F-18's, used for larger scale projects. The T-34C, built by Beech, carries a crew of 2 and is nicknamed the Mentor. June 20, 2005 NASA / Photo Jim Ross EC05-0133-08 |
Date |
10/10/08 |
|
Beech T-34C is Flown by NASA
Chase aircraft such as the T
10/10/08
Description |
Chase aircraft such as the T-34C accompany research flights for photography and video purposes. They also provide support for safety and research. At Dryden, the T-34 is used mainly for smaller remotely piloted vehicles which fly slower than NASA's F-18's, used for larger scale projects. The T-34C, built by Beech, carries a crew of 2 and is nicknamed the Mentor. June 20, 2005 NASA / Photo Jim Ross EC05-0133-03 |
Date |
10/10/08 |
|
Power Beaming
EC02-0232-4 Dryden Model Sho
10/01/02
Description |
EC02-0232-4 Dryden Model Shop's Tony Frakowiak remotely flies an experimental model aircraft being powered by a spotlight operated by Dryden aerospace engineer code RA Ryan Warner. October 1, 2002 NASA Photo / Tom Tschida Power Beaming Project Description |
Date |
10/01/02 |
|
NASA Dryden T-38 Flies Low-l
NASA Dryden engineer and pho
7/6/09
Description |
NASA Dryden engineer and photographer Tom Bunce captured one of NASA's T-38 mission support aircraft flown by NASA research pilots Troy Asher and Mark Pestana as they made a low-level flyby over the town of Tehachapi, Calif., during a recent pilot proficiency flight. (Photo courtesy of Tom Bunce) |
Date |
7/6/09 |
|
RAGE experiment package on N
ED09-0183-12 The RAGE experi
8/7/09
Description |
ED09-0183-12 The RAGE experiment package, attached to the black Propulsion Flight Test Fixture, ready to fly on NASA Dryden's F-15B. July 14, 2009 NASA photo / Tony Landis |
Date |
8/7/09 |
|
United We Serve -- Walt Bask
The spirit of volunteerism i
8/11/09
Description |
The spirit of volunteerism is a marriage of two periods in Walt Baskin's life. One provided material for the show, the other showed a sense of reward that comes from helping the children that see it. From that, Baskin, who works in the Atmospheric Science Data Center, has spun a life away from Langley that includes time in classrooms spent teaching aeronautics and physics by combining instruction with entertainment. The Cub Scouts and, now, Boy Scouts, appreciate it, too. The first period of inspiration came when Baskin was a cadet at Virginia Military Institute. "Two professors went on the road with all of these fantastic demonstrations," he said. "I was fascinated by it. Col. (Richard Bryant) Minnix, who was in his 60s, would get on a skateboard, put on a helmet and get a fire extinguisher and blast himself across the stage." What better way to demonstration jet propulsion? "I thought it was great and the kids loved it," Baskin said. The second period came when he was in the Air Force. "I got involved with the civil air patrol as a mission pilot," he said. Among other things, the CAP flies search and rescue operations. "They also had this cadet program," Baskin said. "It was a dual thing. They had a military side and also aerospace education: the history of flight, how rockets fly, how jets fly and navigate." He was in his mid-20s, and a spark was lit that has yet to be extinguished. When son Andrew, now 12, was younger, Baskin hit upon an idea to bring physics to an elementary school classroom. He called Langley's Outreach office to see if a space suit was available. Told it was, he donned it and went into the classroom, immediately piquing enthusiasm among the tots. With their attention, he used simple demonstrations of physics and meteorology to get his point across. Same with the Cub Scouts. "They were looking for a new leader for the pack," Baskin said. "I had showed up in a spacesuit as a parent to a pack meeting and ended up serving as Packmaster for two years." This was no ordinary Pinewood Derby packmaster. "I did not always use the standard Cub Scout things," Baskin said. "I would bring props and equipment to talk about tornados, about how planes fly, how steam engines work. They loved that." There were experiments, some good, others, well . . . "One was terrible," he said, laughing. "I tried to use Cub Scouts to simulate a cold front. Some scouts were cold air, some were warm air, and it turned into this huge pile of wrestling kids. I said, 'Well, we're not going to do that again.'" Andrew is in Boy Scout Troop 94 now, and dad has drawn back slightly, but certainly not permanently. He's a merit badge counselor in meteorology, aeronautics and other courses for Troop 94. "Pioneering is one of my favorites," Baskin said. "It's engineering in the woods." And he knows the next step is coming. "I suspect within the next few weeks, I'll be an assistant scoutmaster," he said. "I mean, I know the call is coming." And the answer will be yes. It always has, when it comes to science and the world around them. Daughter Madison, 9, has just moved up from Brownies and Girl Scouts, and it's likely that a phone call will come from them, too. Baskin will answer it. It's what he does. Jim Hodges The Researcher News |
Date |
8/11/09 |
|
Artist Concept of X-43A/Hype
Title |
Artist Concept of X-43A/Hyper-X Hypersonic Experimental Research Vehicle in Flight |
Description |
An artist's conception of the X-43A Hypersonic Experimental Vehicle, or "Hyper-X" in flight. The X-43A was developed to flight test a dual-mode ramjet/scramjet propulsion system at speeds from Mach 7 up to Mach 10 (7 to 10 times the speed of sound, which varies with temperature and altitude). Hyper-X, the flight vehicle for which is designated as X-43A, is an experimental flight-research program seeking to demonstrate airframe-integrated, "air-breathing" engine technologies that promise to increase payload capacity for future vehicles, including hypersonic aircraft (faster than Mach 5) and reusable space launchers. This multiyear program is currently underway at NASA Dryden Flight Research Center, Edwards, California. The Hyper-X schedule calls for its first flight later this year (2000). Hyper-X is a joint program, with Dryden sharing responsibility with NASA's Langley Research Center, Hampton, Virginia. Dryden's primary role is to fly three unpiloted X-43A research vehicles to validate engine technologies and hypersonic design tools as well as the hypersonic test facility at Langley. Langley manages the program and leads the technology development effort. The Hyper-X Program seeks to significantly expand the speed boundaries of air-breathing propulsion by being the first aircraft to demonstrate an airframe-integrated, scramjet-powered free flight. Scramjets (supersonic-combustion ramjets) are ramjet engines in which the airflow through the whole engine remains supersonic. Scramjet technology is challenging because only limited testing can be performed in ground facilities. Long duration, full-scale testing requires flight research. Scramjet engines are air-breathing, capturing their oxygen from the atmosphere. Current spacecraft, such as the Space Shuttle, are rocket powered, so they must carry both fuel and oxygen for propulsion. Scramjet technology-based vehicles need to carry only fuel. By eliminating the need to carry oxygen, future hypersonic vehicles will be able to carry heavier payloads. Another unique aspect of the X-43A vehicle is the airframe integration. The body of the vehicle itself forms critical elements of the engine. The forebody acts as part of the intake for airflow and the aft section serves as the nozzle. The X-43A vehicles were manufactured by Micro Craft, Inc., Tullahoma, Tennessee. Orbital Sciences Corporation, Chandler, Arizona, built the Pegasus rocket booster used to launch the X-43 vehicles. For the Dryden research flights, the Pegasus rocket booster and attached X-43 will be air launched by Dryden's B-52 "Mothership." After release from the B-52, the booster will accelerate the X-43A vehicle to the established test conditions (Mach 7 to 10) at an altitude of approximately 100,000 feet where the X-43 will separate from the booster and fly under its own power and preprogrammed control. |
Date |
01.01.1998 |
|
Hyper-X Research Vehicle - A
Title |
Hyper-X Research Vehicle - Artist Concept in Flight |
Description |
An artist's conception of the X-43A Hypersonic Experimental Vehicle, or "Hyper-X" in flight. The X-43A was developed to flight test a dual-mode ramjet/scramjet propulsion system at speeds from Mach 7 up to Mach 10 (7 to 10 times the speed of sound, which varies with temperature and altitude). Hyper-X, the flight vehicle for which is designated as X-43A, is an experimental flight-research program seeking to demonstrate airframe-integrated, "air-breathing" engine technologies that promise to increase payload capacity for future vehicles, including hypersonic aircraft (faster than Mach 5) and reusable space launchers. This multiyear program is currently underway at NASA Dryden Flight Research Center, Edwards, California. The Hyper-X schedule calls for its first flight later this year (2000). Hyper-X is a joint program, with Dryden sharing responsibility with NASA's Langley Research Center, Hampton, Virginia. Dryden's primary role is to fly three unpiloted X-43A research vehicles to validate engine technologies and hypersonic design tools as well as the hypersonic test facility at Langley. Langley manages the program and leads the technology development effort. The Hyper-X Program seeks to significantly expand the speed boundaries of air-breathing propulsion by being the first aircraft to demonstrate an airframe-integrated, scramjet-powered free flight. Scramjets (supersonic-combustion ramjets) are ramjet engines in which the airflow through the whole engine remains supersonic. Scramjet technology is challenging because only limited testing can be performed in ground facilities. Long duration, full-scale testing requires flight research. Scramjet engines are air-breathing, capturing their oxygen from the atmosphere. Current spacecraft, such as the Space Shuttle, are rocket powered, so they must carry both fuel and oxygen for propulsion. Scramjet technology-based vehicles need to carry only fuel. By eliminating the need to carry oxygen, future hypersonic vehicles will be able to carry heavier payloads. Another unique aspect of the X-43A vehicle is the airframe integration. The body of the vehicle itself forms critical elements of the engine. The forebody acts as part of the intake for airflow and the aft section serves as the nozzle. The X-43A vehicles were manufactured by Micro Craft, Inc., Tullahoma, Tennessee. Orbital Sciences Corporation, Chandler, Arizona, built the Pegasus rocket booster used to launch the X-43 vehicles. For the Dryden research flights, the Pegasus rocket booster and attached X-43 will be air launched by Dryden's B-52 "Mothership." After release from the B-52, the booster will accelerate the X-43A vehicle to the established test conditions (Mach 7 to 10) at an altitude of approximately 100,000 feet where the X-43 will separate from the booster and fly under its own power and preprogrammed control. |
Date |
01.01.1997 |
|
Hyper-X Vehicle Model - Fron
Title |
Hyper-X Vehicle Model - Front View |
Description |
A front view of an early desk-top model of NASA's X-43A "Hyper-X," or Hypersonic Experimental Vehicle, which has been developed to flight test a dual-mode ramjet/scramjet propulsion system at speeds from Mach 7 up to Mach 10 (7 to 10 times the speed of sound, which varies with temperature and altitude). Hyper-X, the flight vehicle for which is designated as X-43A, is an experimental flight-research program seeking to demonstrate airframe-integrated, "air-breathing" engine technologies that promise to increase payload capacity for future vehicles, including hypersonic aircraft (faster than Mach 5) and reusable space launchers. This multiyear program is currently underway at NASA Dryden Flight Research Center, Edwards, California. The Hyper-X schedule calls for its first flight later this year (2000). Hyper-X is a joint program, with Dryden sharing responsibility with NASA's Langley Research Center, Hampton, Virginia. Dryden's primary role is to fly three unpiloted X-43A research vehicles to validate engine technologies and hypersonic design tools as well as the hypersonic test facility at Langley. Langley manages the program and leads the technology development effort. The Hyper-X Program seeks to significantly expand the speed boundaries of air-breathing propulsion by being the first aircraft to demonstrate an airframe-integrated, scramjet-powered free flight. Scramjets (supersonic-combustion ramjets) are ramjet engines in which the airflow through the whole engine remains supersonic. Scramjet technology is challenging because only limited testing can be performed in ground facilities. Long duration, full-scale testing requires flight research. Scramjet engines are air-breathing, capturing their oxygen from the atmosphere. Current spacecraft, such as the Space Shuttle, are rocket powered, so they must carry both fuel and oxygen for propulsion. Scramjet technology-based vehicles need to carry only fuel. By eliminating the need to carry oxygen, future hypersonic vehicles will be able to carry heavier payloads. Another unique aspect of the X-43A vehicle is the airframe integration. The body of the vehicle itself forms critical elements of the engine. The forebody acts as part of the intake for airflow and the aft section serves as the nozzle. The X-43A vehicles were manufactured by Micro Craft, Inc., Tullahoma, Tennessee. Orbital Sciences Corporation, Chandler, Arizona, built the Pegasus rocket booster used to launch the X-43 vehicles. For the Dryden research flights, the Pegasus rocket booster and attached X-43 will be air launched by Dryden's B-52 "Mothership." After release from the B-52, the booster will accelerate the X-43A vehicle to the established test conditions (Mach 7 to 10) at an altitude of approximately 100,000 feet where the X-43 will separate from the booster and fly under its own power and preprogrammed control. |
Date |
08.01.1996 |
|
Hyper-X Vehicle Model - Side
Title |
Hyper-X Vehicle Model - Side View |
Description |
A side-view of an early desk-top model of NASA's X-43A "Hyper-X," or Hypersonic Experimental Vehicle, which has been developed to flight test a dual-mode ramjet/scramjet propulsion system at speeds from Mach 7 up to Mach 10 (7 to 10 times the speed of sound, which varies with temperature and altitude). Hyper-X, the flight vehicle for which is designated as X-43A, is an experimental flight-research program seeking to demonstrate airframe-integrated, "air-breathing" engine technologies that promise to increase payload capacity for future vehicles, including hypersonic aircraft (faster than Mach 5) and reusable space launchers. This multiyear program is currently underway at NASA Dryden Flight Research Center, Edwards, California. The Hyper-X schedule calls for its first flight later this year (2000). Hyper-X is a joint program, with Dryden sharing responsibility with NASA's Langley Research Center, Hampton, Virginia. Dryden's primary role is to fly three unpiloted X-43A research vehicles to validate engine technologies and hypersonic design tools as well as the hypersonic test facility at Langley. Langley manages the program and leads the technology development effort. The Hyper-X Program seeks to significantly expand the speed boundaries of air-breathing propulsion by being the first aircraft to demonstrate an airframe-integrated, scramjet-powered free flight. Scramjets (supersonic-combustion ramjets) are ramjet engines in which the airflow through the whole engine remains supersonic. Scramjet technology is challenging because only limited testing can be performed in ground facilities. Long duration, full-scale testing requires flight research. Scramjet engines are air-breathing, capturing their oxygen from the atmosphere. Current spacecraft, such as the Space Shuttle, are rocket powered, so they must carry both fuel and oxygen for propulsion. Scramjet technology-based vehicles need to carry only fuel. By eliminating the need to carry oxygen, future hypersonic vehicles will be able to carry heavier payloads. Another unique aspect of the X-43A vehicle is the airframe integration. The body of the vehicle itself forms critical elements of the engine. The forebody acts as part of the intake for airflow and the aft section serves as the nozzle. The X-43A vehicles were manufactured by Micro Craft, Inc., Tullahoma, Tennessee. Orbital Sciences Corporation, Chandler, Arizona, built the Pegasus rocket booster used to launch the X-43 vehicles. For the Dryden research flights, the Pegasus rocket booster and attached X-43 will be air launched by Dryden's B-52 "Mothership." After release from the B-52, the booster will accelerate the X-43A vehicle to the established test conditions (Mach 7 to 10) at an altitude of approximately 100,000 feet where the X-43 will separate from the booster and fly under its own power and preprogrammed control. |
Date |
08.01.1996 |
|
X-43A Hypersonic Experimenta
Title |
X-43A Hypersonic Experimental Vehicle - Artist Concept in Flight |
Description |
An artist's conception of the X-43A Hypersonic Experimental Vehicle, or "Hyper-X" in flight. The X-43A was developed to flight test a dual-mode ramjet/scramjet propulsion system at speeds from Mach 7 up to Mach 10 (7 to 10 times the speed of sound, which varies with temperature and altitude). Hyper-X, the flight vehicle for which is designated as X-43A, is an experimental flight-research program seeking to demonstrate airframe-integrated, "air-breathing" engine technologies that promise to increase payload capacity for future vehicles, including hypersonic aircraft (faster than Mach 5) and reusable space launchers. This multiyear program is currently underway at NASA Dryden Flight Research Center, Edwards, California. The Hyper-X schedule calls for its first flight later this year (2000). Hyper-X is a joint program, with Dryden sharing responsibility with NASA's Langley Research Center, Hampton, Virginia. Dryden's primary role is to fly three unpiloted X-43A research vehicles to validate engine technologies and hypersonic design tools as well as the hypersonic test facility at Langley. Langley manages the program and leads the technology development effort. The Hyper-X Program seeks to significantly expand the speed boundaries of air-breathing propulsion by being the first aircraft to demonstrate an airframe-integrated, scramjet-powered free flight. Scramjets (supersonic-combustion ramjets) are ramjet engines in which the airflow through the whole engine remains supersonic. Scramjet technology is challenging because only limited testing can be performed in ground facilities. Long duration, full-scale testing requires flight research. Scramjet engines are air-breathing, capturing their oxygen from the atmosphere. Current spacecraft, such as the Space Shuttle, are rocket powered, so they must carry both fuel and oxygen for propulsion. Scramjet technology-based vehicles need to carry only fuel. By eliminating the need to carry oxygen, future hypersonic vehicles will be able to carry heavier payloads. Another unique aspect of the X-43A vehicle is the airframe integration. The body of the vehicle itself forms critical elements of the engine. The forebody acts as part of the intake for airflow and the aft section serves as the nozzle. The X-43A vehicles were manufactured by Micro Craft, Inc., Tullahoma, Tennessee. Orbital Sciences Corporation, Chandler, Arizona, built the Pegasus rocket booster used to launch the X-43 vehicles. For the Dryden research flights, the Pegasus rocket booster and attached X-43 will be air launched by Dryden's B-52 "Mothership." After release from the B-52, the booster will accelerate the X-43A vehicle to the established test conditions (Mach 7 to 10) at an altitude of approximately 100,000 feet where the X-43 will separate from the booster and fly under its own power and preprogrammed control. |
Date |
01.01.1999 |
|
X-43A Undergoing Controlled
Title |
X-43A Undergoing Controlled Radio Frequency Testing in the Benefield Anechoic Facility at Edwards Ai |
Description |
The X-43A Hypersonic Experimental (Hyper-X) Vehicle hangs suspended in the cavernous Benefield Aenechoic Facility at Edwards Air Force Base during radio frequency tests in January 2000. Hyper-X, the flight vehicle for which is designated as X-43A, is an experimental flight-research program seeking to demonstrate airframe-integrated, "air-breathing" engine technologies that promise to increase payload capacity for future vehicles, including hypersonic aircraft (faster than Mach 5) and reusable space launchers. This multiyear program is currently underway at NASA Dryden Flight Research Center, Edwards, California. The Hyper-X schedule calls for its first flight later this year (2000). Hyper-X is a joint program, with Dryden sharing responsibility with NASA's Langley Research Center, Hampton, Virginia. Dryden's primary role is to fly three unpiloted X-43A research vehicles to validate engine technologies and hypersonic design tools as well as the hypersonic test facility at Langley. Langley manages the program and leads the technology development effort. The Hyper-X Program seeks to significantly expand the speed boundaries of air-breathing propulsion by being the first aircraft to demonstrate an airframe-integrated, scramjet-powered free flight. Scramjets (supersonic-combustion ramjets) are ramjet engines in which the airflow through the whole engine remains supersonic. Scramjet technology is challenging because only limited testing can be performed in ground facilities. Long duration, full-scale testing requires flight research. Scramjet engines are air-breathing, capturing their oxygen from the atmosphere. Current spacecraft, such as the Space Shuttle, are rocket powered, so they must carry both fuel and oxygen for propulsion. Scramjet technology-based vehicles need to carry only fuel. By eliminating the need to carry oxygen, future hypersonic vehicles will be able to carry heavier payloads. Another unique aspect of the X-43A vehicle is the airframe integration. The body of the vehicle itself forms critical elements of the engine. The forebody acts as part of the intake for airflow and the aft section serves as the nozzle. The X-43A vehicles were manufactured by Micro Craft, Inc., Tullahoma, Tennessee. Orbital Sciences Corporation, Chandler, Arizona, built the Pegasus rocket booster used to launch the X-43 vehicles. For the Dryden research flights, the Pegasus rocket booster and attached X-43 will be air launched by Dryden's B-52 "Mothership." After release from the B-52, the booster will accelerate the X-43A vehicle to the established test conditions (Mach 7 to 10) at an altitude of approximately 100,000 feet where the X-43 will separate from the booster and fly under its own power and preprogrammed control. |
Date |
01.01.2000 |
|
X-43A Undergoing Controlled
Title |
X-43A Undergoing Controlled Radio Frequency Testing in the Benefield Anechoic Facility at Edwards Ai |
Description |
The X-43A Hypersonic Experimental (Hyper-X) Vehicle hangs suspended in the cavernous Benefield Aenechoic Facility at Edwards Air Force Base during radio frequency tests in January 2000. Hyper-X, the flight vehicle for which is designated as X-43A, is an experimental flight-research program seeking to demonstrate airframe-integrated, "air-breathing" engine technologies that promise to increase payload capacity for future vehicles, including hypersonic aircraft (faster than Mach 5) and reusable space launchers. This multiyear program is currently underway at NASA Dryden Flight Research Center, Edwards, California. The Hyper-X schedule calls for its first flight later this year (2000). Hyper-X is a joint program, with Dryden sharing responsibility with NASA's Langley Research Center, Hampton, Virginia. Dryden's primary role is to fly three unpiloted X-43A research vehicles to validate engine technologies and hypersonic design tools as well as the hypersonic test facility at Langley. Langley manages the program and leads the technology development effort. The Hyper-X Program seeks to significantly expand the speed boundaries of air-breathing propulsion by being the first aircraft to demonstrate an airframe-integrated, scramjet-powered free flight. Scramjets (supersonic-combustion ramjets) are ramjet engines in which the airflow through the whole engine remains supersonic. Scramjet technology is challenging because only limited testing can be performed in ground facilities. Long duration, full-scale testing requires flight research. Scramjet engines are air-breathing, capturing their oxygen from the atmosphere. Current spacecraft, such as the Space Shuttle, are rocket powered, so they must carry both fuel and oxygen for propulsion. Scramjet technology-based vehicles need to carry only fuel. By eliminating the need to carry oxygen, future hypersonic vehicles will be able to carry heavier payloads. Another unique aspect of the X-43A vehicle is the airframe integration. The body of the vehicle itself forms critical elements of the engine. The forebody acts as part of the intake for airflow and the aft section serves as the nozzle. The X-43A vehicles were manufactured by Micro Craft, Inc., Tullahoma, Tennessee. Orbital Sciences Corporation, Chandler, Arizona, built the Pegasus rocket booster used to launch the X-43 vehicles. For the Dryden research flights, the Pegasus rocket booster and attached X-43 will be air launched by Dryden's B-52 "Mothership." After release from the B-52, the booster will accelerate the X-43A vehicle to the established test conditions (Mach 7 to 10) at an altitude of approximately 100,000 feet where the X-43 will separate from the booster and fly under its own power and preprogrammed control. |
Date |
01.01.2000 |
|
X-43A Undergoing Controlled
Title |
X-43A Undergoing Controlled Radio Frequency Testing in the Benefield Anechoic Facility at Edwards Ai |
Description |
The X-43A Hypersonic Experimental (Hyper-X) Vehicle hangs suspended in the cavernous Benefield Aenechoic Facility at Edwards Air Force Base during radio frequency tests in January 2000. Hyper-X, the flight vehicle for which is designated as X-43A, is an experimental flight-research program seeking to demonstrate airframe-integrated, "air-breathing" engine technologies that promise to increase payload capacity for future vehicles, including hypersonic aircraft (faster than Mach 5) and reusable space launchers. This multiyear program is currently underway at NASA Dryden Flight Research Center, Edwards, California. The Hyper-X schedule calls for its first flight later this year (2000). Hyper-X is a joint program, with Dryden sharing responsibility with NASA's Langley Research Center, Hampton, Virginia. Dryden's primary role is to fly three unpiloted X-43A research vehicles to validate engine technologies and hypersonic design tools as well as the hypersonic test facility at Langley. Langley manages the program and leads the technology development effort. The Hyper-X Program seeks to significantly expand the speed boundaries of air-breathing propulsion by being the first aircraft to demonstrate an airframe-integrated, scramjet-powered free flight. Scramjets (supersonic-combustion ramjets) are ramjet engines in which the airflow through the whole engine remains supersonic. Scramjet technology is challenging because only limited testing can be performed in ground facilities. Long duration, full-scale testing requires flight research. Scramjet engines are air-breathing, capturing their oxygen from the atmosphere. Current spacecraft, such as the Space Shuttle, are rocket powered, so they must carry both fuel and oxygen for propulsion. Scramjet technology-based vehicles need to carry only fuel. By eliminating the need to carry oxygen, future hypersonic vehicles will be able to carry heavier payloads. Another unique aspect of the X-43A vehicle is the airframe integration. The body of the vehicle itself forms critical elements of the engine. The forebody acts as part of the intake for airflow and the aft section serves as the nozzle. The X-43A vehicles were manufactured by Micro Craft, Inc., Tullahoma, Tennessee. Orbital Sciences Corporation, Chandler, Arizona, built the Pegasus rocket booster used to launch the X-43 vehicles. For the Dryden research flights, the Pegasus rocket booster and attached X-43 will be air launched by Dryden's B-52 "Mothership." After release from the B-52, the booster will accelerate the X-43A vehicle to the established test conditions (Mach 7 to 10) at an altitude of approximately 100,000 feet where the X-43 will separate from the booster and fly under its own power and preprogrammed control. |
Date |
01.01.2000 |
|
X-43A Undergoing Controlled
Title |
X-43A Undergoing Controlled Radio Frequency Testing in the Benefield Anechoic Facility at Edwards Ai |
Description |
The X-43A Hypersonic Experimental (Hyper-X) Vehicle hangs suspended in the cavernous Benefield Aenechoic Facility at Edwards Air Force Base during radio frequency tests in January 2000. Hyper-X, the flight vehicle for which is designated as X-43A, is an experimental flight-research program seeking to demonstrate airframe-integrated, "air-breathing" engine technologies that promise to increase payload capacity for future vehicles, including hypersonic aircraft (faster than Mach 5) and reusable space launchers. This multiyear program is currently underway at NASA Dryden Flight Research Center, Edwards, California. The Hyper-X schedule calls for its first flight later this year (2000). Hyper-X is a joint program, with Dryden sharing responsibility with NASA's Langley Research Center, Hampton, Virginia. Dryden's primary role is to fly three unpiloted X-43A research vehicles to validate engine technologies and hypersonic design tools as well as the hypersonic test facility at Langley. Langley manages the program and leads the technology development effort. The Hyper-X Program seeks to significantly expand the speed boundaries of air-breathing propulsion by being the first aircraft to demonstrate an airframe-integrated, scramjet-powered free flight. Scramjets (supersonic-combustion ramjets) are ramjet engines in which the airflow through the whole engine remains supersonic. Scramjet technology is challenging because only limited testing can be performed in ground facilities. Long duration, full-scale testing requires flight research. Scramjet engines are air-breathing, capturing their oxygen from the atmosphere. Current spacecraft, such as the Space Shuttle, are rocket powered, so they must carry both fuel and oxygen for propulsion. Scramjet technology-based vehicles need to carry only fuel. By eliminating the need to carry oxygen, future hypersonic vehicles will be able to carry heavier payloads. Another unique aspect of the X-43A vehicle is the airframe integration. The body of the vehicle itself forms critical elements of the engine. The forebody acts as part of the intake for airflow and the aft section serves as the nozzle. The X-43A vehicles were manufactured by Micro Craft, Inc., Tullahoma, Tennessee. Orbital Sciences Corporation, Chandler, Arizona, built the Pegasus rocket booster used to launch the X-43 vehicles. For the Dryden research flights, the Pegasus rocket booster and attached X-43 will be air launched by Dryden's B-52 "Mothership." After release from the B-52, the booster will accelerate the X-43A vehicle to the established test conditions (Mach 7 to 10) at an altitude of approximately 100,000 feet where the X-43 will separate from the booster and fly under its own power and preprogrammed control. |
Date |
01.01.2000 |
|
Photo Description |
The second X-43A hypersonic research vehicle, mounted under the right wing of the B-52B launch aircraft, viewed from the B-52 cockpit. The crew is working on closing out the research vehicle, preparing it for flight. |
Project Description |
The high-risk, high-payoff X-43A flights are the first actual flight tests of an aircraft powered by a scramjet engine capable of operating at hypersonic speeds (above Mach 5, or five times the speed of sound). The X-43A is powered by a revolutionary air-breathing supersonic-combustion ramjet or "scramjet" engine. In a combined research effort involving Dryden, Langley, and several industry partners, NASA demonstrated the value of its X-43A hypersonic research aircraft, as it became the first air-breathing, unpiloted, scramjet-powered plane to fly freely by itself. The March 27 flight, originating from NASA's Dryden Flight Research Center, began with the Agency's B-52B launch aircraft carrying the X-43A out to the test range over the Pacific Ocean off the California coast. The X-43A was boosted up to its test altitude of about 95,000 feet, where it separated from its modified Pegasus booster and flew freely under its own power. Two very significant aviation milestones occurred during this test flight: first, controlled accelerating flight at Mach 7 under scramjet power, and second, the successful stage separation at high dynamic pressure of two non-axisymmetric vehicles. To top it all off, the flight resulted in the setting of a new aeronautical speed record. The X-43A reached a speed of over Mach 7, or about 5,000 miles per hour faster than any known aircraft powered by an air-breathing engine has ever flown. |
Photo Date |
March 27, 2004 |
|
Photo Description |
NASA's B-52B launch aircraft at sunset with the second X-43A hypersonic research vehicle attached to a modified Pegasus rocket under its right wing. |
Project Description |
The high-risk, high-payoff X-43A flights are the first actual flight tests of an aircraft powered by a scramjet engine capable of operating at hypersonic speeds (above Mach 5, or five times the speed of sound). The X-43A is powered by a revolutionary air-breathing supersonic-combustion ramjet or "scramjet" engine. In a combined research effort involving Dryden, Langley, and several industry partners, NASA demonstrated the value of its X-43A hypersonic research aircraft, as it became the first air-breathing, unpiloted, scramjet-powered plane to fly freely by itself. The March 27 flight, originating from NASA's Dryden Flight Research Center, began with the Agency's B-52B launch aircraft carrying the X-43A out to the test range over the Pacific Ocean off the California coast. The X-43A was boosted up to its test altitude of about 95,000 feet, where it separated from its modified Pegasus booster and flew freely under its own power. Two very significant aviation milestones occurred during this test flight: first, controlled accelerating flight at Mach 7 under scramjet power, and second, the successful stage separation at high dynamic pressure of two non-axisymmetric vehicles. To top it all off, the flight resulted in the setting of a new aeronautical speed record. The X-43A reached a speed of over Mach 7, or about 5,000 miles per hour faster than any known aircraft powered by an air-breathing engine has ever flown. |
Photo Date |
March 26, 2004 |
|
Photo Description |
The Hyper-X X-43A project team in front of NASA's B-52B launch aircraft with the Pegasus booster and X-43A vehicle attached. |
Project Description |
The high-risk, high-payoff X-43A flights are the first actual flight tests of an aircraft powered by a scramjet engine capable of operating at hypersonic speeds (above Mach 5, or five times the speed of sound). The X-43A is powered by a revolutionary air-breathing supersonic-combustion ramjet or "scramjet" engine. In a combined research effort involving Dryden, Langley, and several industry partners, NASA demonstrated the value of its X-43A hypersonic research aircraft, as it became the first air-breathing, unpiloted, scramjet-powered plane to fly freely by itself. The March 27 flight, originating from NASA's Dryden Flight Research Center, began with the Agency's B-52B launch aircraft carrying the X-43A out to the test range over the Pacific Ocean off the California coast. The X-43A was boosted up to its test altitude of about 95,000 feet, where it separated from its modified Pegasus booster and flew freely under its own power. Two very significant aviation milestones occurred during this test flight: first, controlled accelerating flight at Mach 7 under scramjet power, and second, the successful stage separation at high dynamic pressure of two non-axisymmetric vehicles. To top it all off, the flight resulted in the setting of a new aeronautical speed record. The X-43A reached a speed of over Mach 7, or about 5,000 miles per hour faster than any known aircraft powered by an air-breathing engine has ever flown. |
Photo Date |
March 23, 2004 |
|
JetStar in flight
Title |
JetStar in flight |
Description |
This 18-second movie clip shows the NASA Dryden Lockheed C-140 JetStar in flight with its pylon-mounted air-turbine-drive system used to gather information on the acoustic characteristics of subscale advanced design propellers. Data was gathered through 28 flush-mounted microphones on the skin of the aircraft. From 1976 to 1987 the NASA Lewis Research Center, Cleveland, Ohio -- today known as the Glenn Research Center -- engaged in research and development of an advanced turboprop concept in partnership with Hamilton Standard, Windsor Locks, Connecticut, the largest manufacturer of propellers in the United States. The Advanced Turboprop Project took its impetus from the energy crisis of the early 1970's and sought to produce swept propeller blades that would increase efficiency and reduce noise. As the project progressed, Pratt & Whitney, Allison Gas Turbine Division of General Motors, General Electric, Gulfstream, Rohr Industries, Boeing, Lockheed, and McDonnell Douglas, among others, also took part. NASA Lewis did the much of the ground research and marshaled the resources of these and other members of the aeronautical community. The team came to include the NASA Ames Research Center, Langley Research Center, and the Ames-Dryden Flight Research Facility (before and after that time, the Dryden Flight Research Center). Together, they brought the propeller to the flight research stage, and the team that worked on the project won the coveted Collier Trophy for its efforts in 1987. To test the acoustics of the propeller the team developed, it mounted propeller models on a C-140 JetStar aircraft fuselage at NASA Dryden. The JetStar was modified with the installation of an air-turbine-drive system. The drive motor, with a test propeller, was mounted on a pylon atop the JetStar. The JetStar was equipped with an array of 28 microphones flush-mounted in the fuselage of the aircraft beneath the propeller. Microphones mounted on the wings and on an accompanying Learjet chase aircraft provided far-field acoustic data. Between May 21, 1981 and August of 1982, the JetStar completed roughly 45 research flights with three different propellers in varying configurations. Dryden engineers analyzed some of the resultant data, while they sent flight tapes to Hamilton Standard, Lewis, and Langley for analysis there. The results indicated a need for noise-reduction technology to keep the noise levels down to the project goals. An improved version of the advanced turboprop underwent flight testing in 1987 on a Gulfstream II over Georgia in 1987. These flight tests verified predictions of a 20- to 30-percent fuel savings. However, with the end of the energy crisis, the need for such savings disappeared, and the Advanced Turboprop Project did not lead to the expected industry-wide adoption of the new propeller systems on transport aircraft. In the 1960s, the same JetStar that was used to test the advanced turboprop had been equipped with an electronic variable-stability, flight-control system. Called then a General Purpose Airborne Simulator (GPAS), the aircraft could duplicate the flight characteristics of a wide variety of advanced aircraft and was used for supersonic transport and general aviation research, and as a training and support system for Space Shuttle Approach and Landing Tests at Dryden in 1977. Over the years, the JetStar has also been used for a variety of other flight research projects, including laminar-flow-control flight tests in the mid-1980s. |
Date |
01.01.1981 |
|
50th Anniversary X-Press Spe
NASA's 50th Anniversary: Fiv
1/7/09
Description |
NASA's 50th Anniversary: Five Decades of Dryden Contributions and Contributors Welcome to this supplement to the X-Press "Happy Anniversary NASA" edition. The 20-page main publication includes profiles of 61 people and 28 projects gathered during a vote by Dryden employees and retirees in March and April of 2008. Originally, a small photo spread was planned for that publication, but there was insufficient room in it to give a true taste of the center's history and contributions to NASA's success. This separate supplement still strains to contain the more than five-decade history of Dryden's myriad contributions and the people who made them. But this separate edition allows more room for showcasing some of Dryden's brightest moments, many of which will be seen for the first time by new employees. It is hoped that these editions will be treasured for the snapshots they provide of the legacy Dryden employees become part of when they work at the center. It is the current group of employees that seeks to take up the mantle, helping Dryden further enrich NASA's efforts to reach for heights in the present and an as-yet-unimagined future. |
Date |
1/7/09 |
|
M2-F1 in flight
Photo Description |
The M2-F1 Lifting Body is seen here under tow by an unseen C-47 at the NASA Flight Research Center (later redesignated the Dryden Flight Research Center), Edwards, California. The low-cost vehicle was the first piloted lifting body to be test flown. The lifting-body concept originated in the mid-1950s at the National Advisory Committee for Aeronautics' Ames Aeronautical Laboratory, Mountain View California. By February 1962, a series of possible shapes had been developed, and R. Dale Reed was working to gain support for a research vehicle. |
Project Description |
The wingless, lifting body aircraft design was initially conceived as a means of landing an aircraft horizontally after atmospheric reentry. The absence of wings would make the extreme heat of re-entry less damaging to the vehicle. In 1962, Dryden management approved a program to build a lightweight, unpowered lifting body as a prototype to flight test the wingless concept. It would look like a "flying bathtub," and was designated the M2-F1, the "M" referring to "manned" and "F" referring to "flight" version. It featured a plywood shell placed over a tubular steel frame crafted at Dryden. Construction was completed in 1963. The first flight tests of the M2-F1 were over Rogers Dry Lake at the end of a tow rope attached to a hopped-up Pontiac convertible driven at speeds up to about 120 mph. These initial tests produced enough flight data about the M2-F1 to proceed with flights behind a NASA C-47 tow plane at greater altitudes. The C-47 took the craft to an altitude of 12,000 where free flights back to Rogers Dry Lake began. Pilot for the first series of flights of the M2-F1 was NASA research pilot Milt Thompson. Typical glide flights with the M2-F1 lasted about two minutes and reached speeds of 110 to 120 mph. More than 400 ground tows and 77 aircraft tow flights were carried out with the M2-F1. The success of Dryden's M2-F1 program led to NASA's development and construction of two heavyweight lifting bodies based on studies at NASA's Ames and Langley research centers--the M2-F2 and the HL-10, both built by the Northrop Corporation, and the U.S. Air Force's X-24 program. The Lifting Body program also heavily influenced the Space Shuttle program. The M2-F1 program demonstrated the feasibility of the lifting-body concept for horizontal landings of atmospheric entry vehicles. It also demonstrated a procurement and management concept for prototype flight research vehicles that produced rapid results at very low cost (approximately $50,000, excluding salaries of government employees assigned to the project). |
Photo Date |
August 28, 1964 |
|
Photo Description |
This image (captured from animation video) illustrates the X-43A research vehicle alone after separation from the Pegasus booster. (LaRC Photo # EL-2000-00531) |
Project Description |
The experimental X-43A hypersonic research aircraft, part aircraft and part spacecraft, will be dropped from the wing of a modified B-52 aircraft, boosted to nearly 100,000 feet altitude by a booster rocket and released over the Pacific Ocean to briefly fly under its own power at seven times the speed of sound, almost 5,000 mph. The flight is part of the Hyper-X program, a research effort designed to demonstrate alternate propulsion technologies for access to space and high-speed flight within the atmosphere. It will provide unique "first time" free flight data on hypersonic air-breathing engine technologies that have large potential pay-offs. The $250 million program began with conceptual design and scramjet engine wind tunnel work in 1996. In a scramjet (supersonic-combustion ramjet), the flow of air through the engine remains supersonic, or greater than the speed of sound, for optimum engine efficiency and vehicle speed. A scramjet operates by supersonic combustion of fuel in a stream of air com,pressed by the high forward speed of the aircraft, as opposed to a normal jet engine, in which the compressor blades compress the air. Scramjets start operation at about Mach 6, or six times the speed of sound. There are few or no moving parts in a scramjet engine, but achieving proper ignition and combustion in a matter of milliseconds proved to be an engineering challenge of the highest order. Researchers believe these technologies may someday offer more airplane-like operations and other benefits compared to traditional rocket systems. Rockets provide limited throttle control and must carry heavy tanks filled with liquid oxygen, necessary for combustion of fuel. An air-breathing engine, like that on the X-43A, scoops oxygen from the air as it flies. The weight savings could be used to increase payload capacity, increase range or reduce vehicle size for the same payload. NASA's Langley Research Center, Hampton, Va., and Dryden Flight Research Center, Edwards, Calif., jointly conduct the Hyper-X program. ATK-GASL (formerly Microcraft, Inc.) of Tullahoma, Tenn., built both the X-43A aircraft and the scramjet engine, and Boeing Phantom Works, Huntington Beach, Calif., designed the thermal protection and onboard systems. The booster is a modified first stage of a Pegasus rocket built by Orbital Sciences Corp, Chandler, Ariz. |
Photo Date |
September 13, 2000 |
|
Photo Description |
This image (captured from animation video) illustrates the separation of the X-43A research vehicle from the Pegasus booster. (LaRC Photo # EL-2000-00532) |
Project Description |
The experimental X-43A hypersonic research aircraft, part aircraft and part spacecraft, will be dropped from the wing of a modified B-52 aircraft, boosted to nearly 100,000 feet altitude by a booster rocket and released over the Pacific Ocean to briefly fly under its own power at seven times the speed of sound, almost 5,000 mph. The flight is part of the Hyper-X program, a research effort designed to demonstrate alternate propulsion technologies for access to space and high-speed flight within the atmosphere. It will provide unique "first time" free flight data on hypersonic air-breathing engine technologies that have large potential pay-offs. The $250 million program began with conceptual design and scramjet engine wind tunnel work in 1996. In a scramjet (supersonic-combustion ramjet), the flow of air through the engine remains supersonic, or greater than the speed of sound, for optimum engine efficiency and vehicle speed. A scramjet operates by supersonic combustion of fuel in a stream of air com,pressed by the high forward speed of the aircraft, as opposed to a normal jet engine, in which the compressor blades compress the air. Scramjets start operation at about Mach 6, or six times the speed of sound. There are few or no moving parts in a scramjet engine, but achieving proper ignition and combustion in a matter of milliseconds proved to be an engineering challenge of the highest order. Researchers believe these technologies may someday offer more airplane-like operations and other benefits compared to traditional rocket systems. Rockets provide limited throttle control and must carry heavy tanks filled with liquid oxygen, necessary for combustion of fuel. An air-breathing engine, like that on the X-43A, scoops oxygen from the air as it flies. The weight savings could be used to increase payload capacity, increase range or reduce vehicle size for the same payload. NASA's Langley Research Center, Hampton, Va., and Dryden Flight Research Center, Edwards, Calif., jointly conduct the Hyper-X program. ATK-GASL (formerly Microcraft, Inc.) of Tullahoma, Tenn., built both the X-43A aircraft and the scramjet engine, and Boeing Phantom Works, Huntington Beach, Calif., designed the thermal protection and onboard systems. The booster is a modified first stage of a Pegasus rocket built by Orbital Sciences Corp, Chandler, Ariz. |
Photo Date |
September 13, 2000 |
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Dryden Center Director
Kevin L. Petersen Director N
3/10/09
Description |
Kevin L. Petersen Director NASA Dryden Flight Research Center Read News Release 09-09 NASA Photo ED07-0126-04 |
Date |
3/10/09 |
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Guppy
EC00-0212-13Members of the f
4/20/09
Description |
EC00-0212-13Members of the flight and ground crews prepare to unload equipment from NASA's B377SGT Super Guppy Turbine cargo aircraft on the ramp at NASA's Dryden Flight Research Center at Edwards Air Force Base, Calif. The outsize cargo plane had delivered the latest version of the X-38 flight test vehicle to NASA Dryden when this photo was taken on June 11, 2000.July 11, 2000NASA Photo / Tony Landis |
Date |
4/20/09 |
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Automatic Collision Avoidanc
ED09-0070-01 The U.S. Air Fo
4/22/09
Description |
ED09-0070-01 The U.S. Air Force's F-16D Automatic Collision Avoidance Technology (ACAT) aircraft cruises during a flight originating from NASA's Dryden Flight Research Center. NASA Dryden is working with the Air Force Research Laboratory in the ACAT Fighter Risk Reduction Project to develop collision avoidance technologies for fighter/attack aircraft that would reduce the risk of ground and mid-air collisions. March 24, 2009 NASA Photo / Jim Ross |
Date |
4/22/09 |
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T-34C in Flight
A NASA T-34C aircraft, used
10/10/08
Description |
A NASA T-34C aircraft, used for safety chase, is shown flying above the Dryden Flight Research Center, Edwards, California in March 1997. The aircraft was previously used at the Lewis Research Center in propulsion experiments involving turboprop engines, and was used as a chase aircraft at Dryden for smaller and slower research projects. March 21, 1997 NASA / Photo EC97-43987-2 |
Date |
10/10/08 |
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Automatic Collision Avoidanc
ED09-0070-27 The U.S. Air Fo
4/22/09
Description |
ED09-0070-27 The U.S. Air Force's F-16D Automatic Collision Avoidance Technology (ACAT) aircraft banks over NASA's Dryden Flight Research Center during a March 2009 flight. NASA Dryden is working with the Air Force Research Laboratory in the ACAT Fighter Risk Reduction Project to develop collision avoidance technologies for fighter/attack aircraft that would reduce the risk of ground and mid-air collisions. March 24, 2009 NASA Photo / Jim Ross |
Date |
4/22/09 |
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Automatic Collision Avoidanc
ED09-0070-29 The U.S. Air Fo
4/22/09
Description |
ED09-0070-29 The U.S. Air Force's F-16D Automatic Collision Avoidance Technology (ACAT) aircraft banks over NASA's Dryden Flight Research Center during a flight in March 2009. NASA Dryden is working with the Air Force Research Laboratory in the ACAT Fighter Risk Reduction Project to develop collision avoidance technologies for fighter/attack aircraft that would reduce the risk of ground and mid-air collisions. March 24, 2009 NASA Photo / Jim Ross |
Date |
4/22/09 |
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Pilot Ed Lewis with T-34C Ai
NASA pilot Ed Lewis with the
10/10/08
Description |
NASA pilot Ed Lewis with the T-34C aircraft on the Dryden Flight Research Center Ramp. The aircraft was previously used at the Lewis Research Center in propulsion experiments involving turboprop engines, and was used as a chase aircraft at Dryden for smaller and slower research projects. March 4, 1998 NASA / Photo Jim Ross EC98-44441-1 |
Date |
10/10/08 |
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Groundbreaking Set for NASA
Read News Release 09-64 Arti
10/5/09
Description |
Read News Release 09-64 Artist's drawing of the new Consolidated Information Technology Center to be constructed at NASA's Dryden Flight Research Center. October 2009 Courtesy of Development One, Inc. |
Date |
10/5/09 |
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Computational Fluid Dynamics
Photo Description |
This computational fluid dynamics (CFD) image shows the Hyper-X vehicle at a Mach 7 test condition with the engine operating. The solution includes both internal (scramjet engine) and external flow fields, including the interaction between the engine exhaust and vehicle aerodynamics. The image illustrates surface heat transfer on the vehicle surface (red is highest heating) and flowfield contours at local Mach number. The last contour illustrates the engine exhaust plume shape. This solution approach is one method of predicting the vehicle performance, and the best method for determination of vehicle structural, pressure and thermal design loads. The Hyper-X program is an ambitious series of experimental flights to expand the boundaries of high-speed aeronautics and develop new technologies for space access. When the first of three aircraft flies, it will be the first time a non-rocket engine has powered a vehicle in flight at hypersonic speeds--speeds above Mach 5, equivalent to about one mile per second or approximately 3,600 miles per hour at sea level. |
Project Description |
Hyper-X, the flight vehicle for which is designated as X-43A, is an experimental flight-research program seeking to demonstrate airframe-integrated, "air-breathing" engine technologies that promise to increase payload capacity for future vehicles, including hypersonic aircraft (faster than Mach 5) and reusable space launchers. This multiyear program is currently underway at NASA Dryden Flight Research Center, Edwards, California. The Hyper-X schedule calls for its first flight later this year (2000). Hyper-X is a joint program, with Dryden sharing responsibility with NASA's Langley Research Center, Hampton, Virginia. Dryden's primary role is to fly three unpiloted X-43A research vehicles to validate engine technologies and hypersonic design tools as well as the hypersonic test facility at Langley. Langley manages the program and leads the technology development effort. The Hyper-X Program seeks to significantly expand the speed boundaries of air-breathing propulsion by being the first aircraft to demonstrate an airframe-integrated, scramjet-powered free flight. Scramjets (supersonic-combustion ramjets) are ramjet engines in which the airflow through the whole engine remains supersonic. Scramjet technology is challenging because only limited testing can be performed in ground facilities. Long duration, full-scale testing requires flight research. Scramjet engines are air-breathing, capturing their oxygen from the atmosphere. Current spacecraft, such as the Space Shuttle, are rocket powered, so they must carry both fuel and oxygen for propulsion. Scramjet technology-based vehicles need to carry only fuel. By eliminating the need to carry oxygen, future hypersonic vehicles will be able to carry heavier payloads. Another unique aspect of the X-43A vehicle is the airframe integration. The body of the vehicle itself forms critical elements of the engine. The forebody acts as part of the intake for airflow and the aft section serves as the nozzle. The X-43A vehicles were manufactured by Micro Craft, Inc., Tullahoma, Tennessee. Orbital Sciences Corporation, Chandler, Arizona, built the Pegasus rocket booster used to launch the X-43 vehicles. For the Dryden research flights, the Pegasus rocket booster and attached X-43 will be air launched by Dryden's B-52 "Mothership." After release from the B-52, the booster will accelerate the X-43A vehicle to the established test conditions (Mach 7 to 10) at an altitude of approximately 100,000 feet where the X-43 will separate from the booster and fly under its own power and preprogrammed control. |
Photo Date |
1997 |
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M2-F2 flight preparation and
M2-F2 experiencing lateral o
Milt Thompson prepares for M
M2-F2 test flight with F5D-1
M2-F2 drop from NB-52A mothe
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