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100-lbf Non-Toxic Storable Liquid Propulsion

Completed TRL 5 (started at 3, targeting 5)

Description

NASA's Road Maps for both Launch and In Space Propulsion call for the development of non-toxic, monopropellant reaction control systems to replace the current toxic hydrazine based systems. The Orion Multi-Purpose Crew Vehicle capsule with twelve 160 pound force (lbf) hydrazine monopropellant thrusters and the Orion Service Module with eight 100lbf NTO/MMH auxiliary propulsion thrusters are obvious insertion candidates. Additionally, the Commercial Crew and Cargo spacecraft have also demonstrated the need for 100lbf class attitude control thrusters with quantities comparable to Orion. Hydrazine replacements, including non-toxic HAN- and ADN-monopropellants, combust at higher temperatures making them incompatible with current Inconel 625 thrusters used in 100lbf engines. With an emphasis on hydrazine replacement increased performance, ease of manufacturing and cost reduction, a "green" 100lbf flight-weight thruster is being developed.

Benefits

NASA applications include reaction control thrusters for the Orion MPCV capsule and service module; 100lbf thrusters in support of Commercial Crew and Cargo spacecraft; Reaction Control Systems for Space Launch System

Non-NASA applications include Commercial Access to Space programs including the lift/space craft programs for SpaceX Falcon/Dragon and Orbital Antares/Cygnus; Satellite insertion and positioning; tactical missile divert and attitude control; auxiliary power generators; and jet engine restarters.

Details

Technology areaPropulsion Systems > Chemical Space Propulsion > Earth Storable Propellants
ProgramSmall Business Innovation Research/Small Business Tech Transfer (SBIR/STTR)
Lead organizationPlasma Processes, LLC, Huntsville, AL
Start date2015-05-19
End date2017-10-24

Project contacts

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How to get involved

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.

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