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Press Fed 25k
TRW LOx/Kerosene rocket engine. Design concept 1960's. 1960's designs for 'big dumb booster'.

Status: Design concept 1960's. Thrust: 245.20 kN (55,123 lbf). Unfuelled mass: 270 kg (590 lb). Specific impulse: 270 s. Specific impulse sea level: 230 s. Diameter: 0.67 m (2.19 ft).

Thrust (sl): 208.800 kN (46,940 lbf). Thrust (sl): 21,296 kgf. Engine: 270 kg (590 lb). Area Ratio: 5. Thrust to Weight Ratio: 92.5925925925926. Coefficient of Thrust vacuum: 0. Coefficient of Thrust sea level: 0.



Country: USA. Propellants: Lox/Kerosene. Agency: TRW.

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