Plug-Nozzle SASSTO
Engine · USA
Original archive entry. The text, images and links below are kept as they were written.
Notional LOx/LH2 rocket engine. Study 1967. Used on SASSTO launch vehicle.
Thrust (sl): 1,231.800 kN (276,920 lbf). Thrust (sl): 125,611 kgf.
Related
- Country
- USA
- Launch Vehicles
- SASSTO
- Propellants
- Lox/LH2
- Stages
- SASSTO stage