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Press Fed
TRW N2O4/MMH rocket engine. Design concept 1960's. 1960's designs for 'big dumb booster'.

Status: Design concept 1960's. Thrust: 17.80 kN (4,002 lbf). Unfuelled mass: 41 kg (90 lb). Specific impulse: 300 s. Diameter: 0.67 m (2.19 ft).

Engine: 41 kg (90 lb). Area Ratio: 98. Thrust to Weight Ratio: 44.3436633912824. Coefficient of Thrust vacuum: 0. Coefficient of Thrust sea level: 0.



Family: Storable liquid. Country: USA. Propellants: N2O4/MMH. Agency: TRW.

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