The Combined Cycle Mode Transition challenge demonstrates autonomous control and establishes performance/operability assessment methodologies for future reusable hypersonic propulsion systems that use turbine engines at slow speeds while transitioning to scramjets for high-speed operations. This challenge addresses the technology barrier of propulsion system mode transition via ground tests.
More »Supports the demonstration of critical enabling technologies for hypersonic vehicles and space access platforms with a live turbine engine and simulated high-speed propulsion system.
More »Organizations Performing Work | Role | Type | Location |
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Glenn Research Center (GRC) | Lead Organization | NASA Center | Cleveland, Ohio |
Langley Research Center (LaRC) | Supporting Organization | NASA Center | Hampton, Virginia |