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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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