Press Fed 1000k
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): 7,834.500 kN (1,761,266 lbf). Thrust (sl): 798,911 kgf. Chamber Pressure: 17.01 bar. Area Ratio: 31. Thrust to Weight Ratio: 0. Coefficient of Thrust vacuum: 10.7215909769459. Coefficient of Thrust sea level: 8.89879097694586.