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Plug-Nozzle SASSTO
Notional LOx/LH2 rocket engine. Study 1967. Used on SASSTO launch vehicle.

Status: Study 1967. Thrust: 1,574.90 kN (354,052 lbf). Specific impulse: 459 s. Specific impulse sea level: 359 s. Burn time: 268 s.

Thrust (sl): 1,231.800 kN (276,920 lbf). Thrust (sl): 125,611 kgf.



Country: USA. Launch Vehicles: SASSTO. Propellants: Lox/LH2. Stages: SASSTO stage.

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