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Electrically-Controlled Extinguishable Solid Propellant

Completed TRL 4 (started at 3, targeting 4)

Description

The development of a safe, electrically-controlled extinguishable solid propellant (ESP) thruster would allow NASA to demonstrate an innovative throttleable solid rocket motor that could replace multi-mode liquid propulsion systems. Replacement of cold gas and monopropellant systems for in-space propulsion with a safe, volumetrically-efficient thruster set could offer game-changing improvements in performance. ESPs are inert unless ignited with an electric potential of appropriate magnitude.

Benefits

These goal of these tests is to demonstrate the feasibility of an electrically-controlled extinguishable solid rocket motor propellant, which could be used as a safe, volumetrically-efficient replacement for liquid thrusters.

Details

Technology areaPropulsion Systems > Chemical Space Propulsion > Solids
ProgramCenter Innovation Fund: MSFC CIF (MSFC CIF)
Lead organizationMarshall Space Flight Center, Huntsville, AL
Start date2012-02-01
End date2012-09-01

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