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Press Fed 200k
TRW N2O4/UDMH rocket engine. Study 1968. 1960's designs for 'big dumb booster'. Used on LCLV launch vehicle.

Status: Study 1968. Thrust: 2,028.00 kN (455,912 lbf). Specific impulse: 306 s. Specific impulse sea level: 200 s. Diameter: 2.90 m (9.50 ft).

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.



Family: Storable liquid. Country: USA. Launch Vehicles: LCLV. Propellants: N2O4/UDMH. Stages: LCLV-3. Agency: TRW.

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