Small Business Innovation Research/Small Business Tech Transfer
Integrated Powerhead for Methane Propulsion Systems
Project Description
Development of an electric powerhead or Electropump for a 25,000 lb class Methane engine. Components for integrated RCS (~100-lb class) and Main Propulsion System (MPS) (25,000-lb class) feed systems (utilizing common propulsion tanks)"
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Anticipated Benefits
enabling technology for Mars Program office, especially for a large lander, as electropump technology is ideal for a deep throttling 5:1 engine. Enabling technology for small spacecraft launch vehicle
small satellite launcher. Mach 10 target launcher for USAF. XS-1 Spacecraft upper stage. More »
small satellite launcher. Mach 10 target launcher for USAF. XS-1 Spacecraft upper stage. More »
Project Library
Primary U.S. Work Locations and Key Partners
| Organizations Performing Work | Role | Type | Location |
|---|---|---|---|
| TGV Rockets, Inc. | Lead Organization |
Industry
Minority-Owned Business,
Small Disadvantaged Business (SDB)
|
Washington, District of Columbia |
Glenn Research Center
(GRC)
|
Supporting Organization | NASA Center | Cleveland, Ohio |
Primary U.S. Work Locations
-
District of Columbia
-
Ohio
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