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Engine · USA
Original archive entry. The text, images and links below are kept as they were written.
TRW LOx/Kerosene rocket engine. Design concept 1960's. 1960's designs for 'big dumb booster'.
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.
Related
- Country
- USA
- Propellants
- Lox/Kerosene
- Agency
- TRW