AJ10-138

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AJ10-138

Part of AJ10

Aerojet N2O4/Aerozine-50 rocket engine. Out of production. Originally developed for Vanguard and Able. Two used, thrust uprated from 3540 kgf to 3628 kgf, with higher specific impulse, in Transtage. Flown 1964-1980.

Status: Out of production. Date: 1958. Number: 80 . Thrust: 35.60 kN (8,003 lbf). Unfuelled mass: 110 kg (240 lb). Specific impulse: 311 s. Burn time: 440 s. Diameter: 1.53 m (5.00 ft).

Engine: 110 kg (240 lb). Chamber Pressure: 7.00 bar. Area Ratio: 40. Thrust to Weight Ratio: 32.9863636363636. Oxidizer to Fuel Ratio: 2. Coefficient of Thrust vacuum: 4.39646147665109.

Family: Storable liquid. Country: USA. Launch Vehicles: Titan IIIC, Titan IIIA, Titan 3C7. Propellants: N2O4/Aerozine-50. Stages: Titan Transtage Stretch, Titan Transtage. Agency: Aerojet.

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