Integrated Powerhead for Methane Propulsion Systems
Status: Completed
Start Date: 2017-06-09
End Date: 2017-12-08
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)"
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.
small satellite launcher. Mach 10 target launcher for USAF. XS-1 Spacecraft upper stage.
Lead Organization: TGV Rockets, Inc.