Press Fed 5748k
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): 51,723.200 kN (11,627,838 lbf). Thrust (sl): 5,274,382 kgf. Chamber Pressure: 20.41 bar. Area Ratio: 6. Thrust to Weight Ratio: 0. Coefficient of Thrust vacuum: 5.59884325570492. Coefficient of Thrust sea level: 5.30484325570492.