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contract
High Mach Gas Turbine (HMGT) Engine Design Study
- Sponsor and partners: Advanced Propulsion Office (APO) with Air Force Research Laboratory (AFRL) and AFLCMC Propulsion Directorate (LP)
- Purpose: Kick-start development of a HMGT engine for future reusable hypersonic aircraft
- Phase 1 focus:
- Conceptual and preliminary engine design
- Subsystem and component testing
- Identify the HMGT engine archite…
Source
Agency: Defense Advanced Research Projects Agency (darpa)
Dates
Response Deadline: November 11, 2025
Keywords
hypersonic propulsion
high-Mach gas turbine
turbine-based combined cycle (TBCC)
reusable hypersonic aircraft
engine core and architecture
subsystem/component testing
high-temperature materials and thermal management
combustor and inlet design for high Mach
AFRL propulsion programs
Air Force propulsion technology roadmap
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