Solid-Fuel Rotating Detonation Ramjet (SF-RDR) for High-Speed Propulsion
SBIR Opportunity Analysis
The Department of Navy is seeking SBIR proposals for a throttleable solid-fuel rotating detonation ramjet system that can improve high-speed propulsion performance and operational flexibility. The work centers on developing a compact, lightweight, throttleable gas generator and optimizing the rotating detonation combustor to support stable detonation propagation and efficient mixing. In Phase I, performers are expected to design and demonstrate a gas generator subsystem that produces a combustible mixture detonable at ramjet-relevant temperatures, with a preferred subscale SFRDE demonstration and sustained detonation for 0.5 to 3.0 seconds after steady state; Phase II would advance a tactical-scale prototype for ground testing under ramjet-relevant conditions and characterize thrust, specific impulse, combustion efficiency, and response time. Proposals are due June 3, 2026 at 16:00 UTC under topic DON26BZ01-NV036.