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Collection:
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NASA Dryden Flight Research Center Collection
Collection
NASA Dryden Flight Research Center Collection
Collection
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Title:
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X-43A / Hyper-X separation from Pegasus and flight - computer animation
Title
X-43A / Hyper-X separation from Pegasus and flight - computer animation
Title
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Description:
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This 32-second video animation shows the flight of the Pegasus¨ launch vehicle with the X-43A attached, the separation of the X-43A and its maneuver and flight above the Pacific Ocean. About midway through the clip, the animation portrays the firing of the scramjet engines in the X-43A vehicle. With a contract awarded to MicroCraft, Inc., Tullahoma, Tennessee, in March of 1997, NASA embarked on a significant new project to demonstrate the use of supersonic combustion ramjet (scramjet) technologies at hypersonic speeds on sub-scale vehicles now known as X-43As. Three of these vehicles are being fabricated at MicroCraft. The Hyper-X Program seeks to demonstrate airframe-integrated, air-breathing engine technologies that promise to increase aircraft speeds and payload capacities for reusable space launchers. Scramjets employ ramjet engines in which the internal airflow remains supersonic. Ramjets operate by combustion of fuel in a stream of air compressed by the forward speed of the vehicle, unlike a normal jet engine in which compressor blades perform that function. Normal ramjets operate with subsonic internal airflow and combustion; they operate from a speed of about Mach 2 to Mach 5. With supersonic combustion, scramjets can operate at speeds faster than the Mach 6.7 speed achieved by the rocket-powered X-15. Scramjets can potentially carry more payload than rockets because they are air-breathing and do not have to carry their own supply of oxygen. This joint program among Langley Research Center, Hampton Virginia, Dryden Flight Research Center, Edwards, California, and industry seeks to fulfill a key NASA goal of providing next-generation design tools and experimental aircraft to increase design confidence and cut the design cycle time for aircraft. Langley has been leading the effort to develop the new technology. Dryden has been responsible for the flight research effort as well as managing the fabrication of the X-43A vehicles and expendable booster rockets that will carry them to speeds of Mach 7 (two flights) and Mach 10 (one flight). The program has also assembled an industrial team providing some of the flight components. These components include the venerable Dryden B-52, which will carry a modified Pegasus¨ (a registered trademark of Orbital Sciences Corporation of Dulles, Virginia) launch vehicle to which the X-43A will be attached. The flights will carry the vehicles over the Sea Test Range off the coast of southern California, where the B-52 will drop the launch vehicle at altitudes ranging between 18,000 and 39,000 feet. The X-43A will be boosted to the respective Mach 7 and Mach 10 speeds, whereupon it will separate from the launch vehicle and demonstrate the scramjet technology. The objectives of the unpiloted flights include: the first-ever free-flight demonstration of an airframe-integrated scramjet; the verification of wind-tunnel tests, computational predictions, and analyses of the technology; and ultimately, the
Description
This 32-second video animation shows the flight of the Pegasus¨ launch vehicle with the X-43A attached, the separation of the X-43A and its maneuver and flight above the Pacific Ocean. About midway through the clip, the animation portrays the firing of the scramjet engines in the X-43A vehicle. With a contract awarded to MicroCraft, Inc., Tullahoma, Tennessee, in March of 1997, NASA embarked on a significant new project to demonstrate the use of supersonic combustion ramjet (scramjet) technologies at hypersonic speeds on sub-scale vehicles now known as X-43As. Three of these vehicles are being fabricated at MicroCraft. The Hyper-X Program seeks to demonstrate airframe-integrated, air-breathing engine technologies that promise to increase aircraft speeds and payload capacities for reusable space launchers. Scramjets employ ramjet engines in which the internal airflow remains supersonic. Ramjets operate by combustion of fuel in a stream of air compressed by the forward speed of the vehicle, unlike a normal jet engine in which compressor blades perform that function. Normal ramjets operate with subsonic internal airflow and combustion; they operate from a speed of about Mach 2 to Mach 5. With supersonic combustion, scramjets can operate at speeds faster than the Mach 6.7 speed achieved by the rocket-powered X-15. Scramjets can potentially carry more payload than rockets because they are air-breathing and do not have to carry their own supply of oxygen. This joint program among Langley Research Center, Hampton Virginia, Dryden Flight Research Center, Edwards, California, and industry seeks to fulfill a key NASA goal of providing next-generation design tools and experimental aircraft to increase design confidence and cut the design cycle time for aircraft. Langley has been leading the effort to develop the new technology. Dryden has been responsible for the flight research effort as well as managing the fabrication of the X-43A vehicles and expendable booster rockets that will carry them to speeds of Mach 7 (two flights) and Mach 10 (one flight). The program has also assembled an industrial team providing some of the flight components. These components include the venerable Dryden B-52, which will carry a modified Pegasus¨ (a registered trademark of Orbital Sciences Corporation of Dulles, Virginia) launch vehicle to which the X-43A will be attached. The flights will carry the vehicles over the Sea Test Range off the coast of southern California, where the B-52 will drop the launch vehicle at altitudes ranging between 18,000 and 39,000 feet. The X-43A will be boosted to the respective Mach 7 and Mach 10 speeds, whereupon it will separate from the launch vehicle and demonstrate the scramjet technology. The objectives of the unpiloted flights include: the first-ever free-flight demonstration of an airframe-integrated scramjet; the verification of wind-tunnel tests, computational predictions, and analyses of the technology; and ultimately, the
Description
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Description:
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scaling of the design concepts to future operational air-breathing hypersonic cruise and space-access vehicles. This effort is challenging because of the limitations on testing in ground facilities and the inherent uncertainties associated with computational methods. Full-scale testing requires flight research.
Description
scaling of the design concepts to future operational air-breathing hypersonic cruise and space-access vehicles. This effort is challenging because of the limitations on testing in ground facilities and the inherent uncertainties associated with computational methods. Full-scale testing requires flight research.
Description
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Movie Date:
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1997
Movie_Date
1997
Movie Date
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note:
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Keywords:
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X-43A
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Keywords:
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Hyper-X
Keywords
Hyper-X
Keywords
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Keywords:
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MicroCraft
Keywords
MicroCraft
Keywords
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Keywords:
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Inc.
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Keywords:
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Langley Research Center
Keywords
Langley Research Center
Keywords
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Keywords:
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Dryden Flight Research Center
Keywords
Dryden Flight Research Center
Keywords
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Keywords:
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NASA
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Keywords:
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supersonic combustion ramjet
Keywords
supersonic combustion ramjet
Keywords
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Keywords:
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scramjet
Keywords
scramjet
Keywords
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Keywords:
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reusable space launchers
Keywords
reusable space launchers
Keywords
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Keywords:
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X-15
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Keywords:
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air-breathing
Keywords
air-breathing
Keywords
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Keywords:
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B-52
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Keywords:
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Pegasus¨
Keywords
Pegasus¨
Keywords
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Keywords:
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Orbital Sciences Corp.
Keywords
Orbital Sciences Corp.
Keywords
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Keywords:
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flight research
Keywords
flight research
Keywords
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Keywords:
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Sea Test Range
Keywords
Sea Test Range
Keywords
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facet_what:
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Pegasus
facet_what
Pegasus
facet_what
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facet_what:
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X-43A
facet_what
X-43A
facet_what
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facet_where:
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California
facet_where
California
facet_where
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facet_where:
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Tennessee
facet_where
Tennessee
facet_where
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facet_where:
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Virginia
facet_where
Virginia
facet_where
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facet_where:
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Pacific Ocean
facet_where
Pacific Ocean
facet_where
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facet_where:
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Dryden Flight Research Center (DFRC)
facet_where
Dryden Flight Research Center (DFRC)
facet_where
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facet_where:
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Langley Research Center (LaRC)
facet_where
Langley Research Center (LaRC)
facet_where
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facet_when:
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1997
facet_when
1997
facet_when
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facet_when_year:
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1997
facet_when_year
1997
facet_when_year
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Movie Number:
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EM-0015-02
Movie_Number
EM-0015-02
Movie Number
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UID:
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SPD-DRYDEN-EM-0015-0 2
UID
SPD-DRYDEN-EM-0015-0 2
UID
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original url:
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original_url
original url
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