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Press Fed 1000k
TRW N2O4/UDMH rocket engine. Study 1968. 1960's designs for 'big dumb booster'. Used on LCLV launch vehicle.

Status: Study 1968. Thrust: 9,793.20 kN (2,201,599 lbf). Specific impulse: 300 s. Specific impulse sea level: 240 s. Diameter: 4.58 m (15.01 ft).

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.



Family: Storable liquid. Country: USA. Launch Vehicles: LCLV. Propellants: N2O4/UDMH. Stages: LCLV-2. Agency: TRW.

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