Operational Demonstration of the MPS-120 CubeSat High-impulse Adaptable Modular Propulsion System
PI: Steve Overton, Aerojet Rocketdyne Holdings Inc
PI: Steve Overton, Aerojet Rocketdyne Holdings Inc
- TA02 In-Space Propulsion Technologies
Propulsive capabilities are required to enable the CubeSat platform to access the wider range of missions that will strengthen the value proposition of the CubeSat platform, ensure continued market growth, and enable reduced cost and schedule NASA missions. Current state of the art cold gas propulsion systems provide DV of ~10 m/s, but DV of >200 m/s is required to enable benefits to NASA and the commercial market.
The program will perform the first operation of Aerojet’s MR-142 miniature hydrazine rocket engine to demonstrate a 4x engine size reduction. The program will also perform the first operation of an additive manufactured piston propellant tank and miniature isolation system that demonstrates safe storage of hydrazine on CubeSats and a credible path to low cost, short lead-time propulsion systems that are not burdened by the operational costs associated with ground handling of hazardous fluids.
NASA
Commercial space
Academia
Technology Details
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Selection DateNRA-2-APP-E (Aug 2013)
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Program StatusWithdrawn
- 0 sRLV
Development Team
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PISteve Overton
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Organization
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SponsorNASA
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More Information