High Mach Gas Turbine (HMGT) Engine Design Study

The High Mach Gas Turbine (HMGT) Engine Design Study is a research and development project aimed at designing a HMGT engine compatible with future reusable hypersonic aircraft. The project is divided into phases, with Phase 1A seeking conceptual and preliminary design efforts, and Phase 1B focusing on subsystem and component testing. The project has a total funding of $10M for Phase 1A and $30M for Phase 1B. The key aspects of the project include identifying the HMGT engine architecture, engine core, required subsystem technologies, and building a technology roadmap to mature each subsystem component technology and the overall engine design. • The project involves conceptual and preliminary design efforts • The project includes subsystem and component testing • The project has a total funding of $40M for Phases 1A and 1B • The project aims to design a HMGT engine compatible with future reusable hypersonic aircraft • The project involves building a technology roadmap to mature each subsystem component technology and the overall engine design