← Back to NASA Technology Projects
Completed TRL 5 (started at 4, targeting 5)
Lunar and Mars missions require Earth-delivered or ISRU-generated cryogenic propellants. Fast-pulse reaction control systems (RCS), haven’t proven reliable ignition. This work will buy down risk by characterizing HLS- & CLPS-class cryogenic RCS ignition systems
Cryogenic propellant systems are considered essential for NASA future human exploration missions1,2, particularly beyond lunar landings (in-situ resource utilization (ISRU), high specific impulse, reduced heating requirements once in space). No cryogenic reaction control system (RCS) has ever flown in space. In previous thermal-vacuum (<-275°F) testing at NASA GRC Plum Brook, the team uncovered anomalous LO2/LCH4 engine ignition phenomena where flame kernels quenched at these ultra-cold hardware temperatures, leading to many pluses where the engines would not light. This work is vital because when the RCEs fire is commanded, and misfires or no-lights this could result in catastrophic vehicle failure. No known complementary projects or efforts are currently underway.
Listed on TechPort itself — the most direct way to ask about this specific project.
This is early/mid-stage (TRL 5) — the most realistic path in is NASA SBIR/STTR, which funds small businesses and research institutions to develop technology aligned with NASA's needs (equity-free, phased funding). Check whether a current SBIR/STTR solicitation topic overlaps with this project's technology area, or contact the project directly (above) to ask.
None of these are guaranteed paths for this specific project — TechPort itself doesn't have an "apply" button. Reaching out to the contact(s) above with a specific question is usually the fastest way to find out what's actually open.