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AJ10-137
Part of AJ10
Aerojet N2O4/Aerozine-50 rocket engine. Apollo SPS. Out of Production. Pressure-fed engine. Used as Apollo SM engine.

Status: Out of Production. Thrust: 97.50 kN (21,919 lbf). Specific impulse: 312 s. Burn time: 585 s.

Chamber Pressure: 6.90 bar. Oxidizer to Fuel Ratio: 1.6.



Family: Storable liquid. Country: USA. Spacecraft: Apollo CSM, Apollo CSM Block I, Apollo RM. Propellants: N2O4/Aerozine-50. Agency: Aerojet.

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