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X-43A airframe-integrated scramjet propulsion system

Historical NASA X-43A Hyper-X airframe-integrated scramjet propulsion system using gaseous hydrogen and atmospheric air, with gaseous silane used as the ignition source. NASA records three unpiloted research vehicles, Mach 6.8 and Mach 9.6 powered flights in 2004, and approximately ten seconds of scramjet operation after booster separation; this row remains the distinct integrated-system identity.

Identity

Aliases
Hyper-X scramjet
Domains
aviation
Identity Level
integrated-system
Kind
scramjet
Name
X-43A airframe-integrated scramjet propulsion system
Status
historical

Details

Description
Historical NASA X-43A Hyper-X airframe-integrated scramjet propulsion system using gaseous hydrogen and atmospheric air, with gaseous silane used as the ignition source. NASA records three unpiloted research vehicles, Mach 6.8 and Mach 9.6 powered flights in 2004, and approximately ten seconds of scramjet operation after booster separation; this row remains the distinct integrated-system identity.
Developers
First Flight Date
2004-03-27
Propellants
gaseous hydrogenatmospheric air
Retirement Date
2004-11-16

Links

Assets & Meta

Creation Time
July 29, 2026 at 07:56:57 UTC
Updated Time
August 22, 2026 at 02:07:54 UTC

Other

Sources
  • Accessed Date
    2026-08-14
    Note
    NASA documents the hydrogen-fueled X-43A airframe-integrated scramjet, the three research vehicles, Mach 6.8 and 9.6 flights, and approximately ten seconds of powered scramjet operation after booster separation.
    Publisher
    NASA
    Title
    X-43A Hyper-X
  • Accessed Date
    2026-08-21
    Note
    The NASA technical report describes the X-43A as a hydrogen-fueled, airframe-integrated scramjet and documents gaseous silane ignition, nitrogen pressurization and inerting, and coolant systems used during the engine test.
    Publisher
    NASA Technical Reports Server
    Title
    A Chief Engineer View of the NASA X-43A Scramjet Flight Test