Plug-Nozzle SERV
Engine · USA
Original archive entry. The text, images and links below are kept as they were written.
Notional LOx/LH2 rocket engine. Study 1971. Used on Shuttle SERV launch vehicle.
Thrust (sl): 25,794.900 kN (5,798,924 lbf). Thrust (sl): 2,630,386 kgf.
Related
- Country
- USA
- Launch Vehicles
- SERV
- Propellants
- Lox/LH2
- Stages
- Shuttle SERV-1