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Engine · USA

Original archive entry. The text, images and links below are kept as they were written.

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

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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