This National Science Foundation (NSF) Technology, Innovation, and Partnerships (CFDA 47.084) Project Grant award provides funding of $274,969 to Juno Propulsion Inc., a small disadvantaged business, to develop a new satellite thruster using rotating detonation combustion (RDC) technology and non-toxic propellants.
The key objectives of this SBIR Phase I project are to: (1) develop an advanced computational modeling tool to predict RDC performance and detonation characteristics, (2) demonstrate RDC functionality for the targeted thrust class and propellant system, and (3) validate the performance benefits of RDC for in-space satellite propulsion applications. By the end of the 12-month project period ending August 2025, the goal is to advance the RDC satellite thruster technology to a higher state of readiness through prototype testing in a relevant vacuum environment. This innovation has the potential to significantly improve satellite lifespan, payload capacity, and performance of critical space-based functions such as imaging, telecommunications, and scientific missions.
Generated 3/4/25, 4:56 AM