Plug-Nozzle SSME
Engine · USA
Original archive entry. The text, images and links below are kept as they were written.
Notional LOx/LH2 rocket engine. Study 1978. Used on VTOVL launch vehicle.
Thrust (sl): 3,167.400 kN (712,060 lbf). Thrust (sl): 322,992 kgf. Engine: 2,973 kg (6,554 lb). Area Ratio: 600. Thrust to Weight Ratio: 127.89.
Related
- Country
- USA
- Launch Vehicles
- VTOVL 1978
- Propellants
- Lox/LH2
- Stages
- VTOVL 150t