Press Fed 200k
Engine · USA
Original archive entry. The text, images and links below are kept as they were written.
TRW N2O4/UDMH rocket engine. Study 1968. 1960's designs for 'big dumb booster'. Used on LCLV launch vehicle.
Thrust (sl): 1,325.500 kN (297,984 lbf). Thrust (sl): 135,165 kgf. Chamber Pressure: 13.61 bar. Area Ratio: 50. Thrust to Weight Ratio: 0. Coefficient of Thrust vacuum: 11.1792052857938. Coefficient of Thrust sea level: 7.50420528579375.