This page no longer updated from 31 October 2001. Latest version can be found at AJ10-137

Manufacturer Name: AJ10-137. Designer: Aerojet. Application: Apollo SPS. Used on spacecraft: Apollo CSM, Apollo CSM + RM. Propellants: N2O4/Aerozine-50 Thrust(vac): 9,900 kgf. Thrust(vac): 97.50 kN. Isp: 312 sec. Burn time: 585 sec. Chambers: 1. Chamber Pressure: 6.90 bar. Oxidizer to Fuel Ratio: 1.60. Country: USA. Status: Out of Production. References: 225 . Comments: Pressure-fed engine. Used as Apollo SM engine.
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Last update 12 March 2001.
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© Mark Wade, 2001 .