AJ10-137

Manufacturer Name: AJ10-137. Designer: Aerojet. Application: Apollo SPS. Propellants: N2O4/Aerozine-50. Thrust(vac): 97.500 kN (21,919 lbf). 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.

Pressure-fed engine. Used as Apollo SM engine.

AJ10-137 used on Spacecraft

Used on: Apollo CSM.

Used on: Apollo CSM Block I.

Used on: Apollo RM.

Bibliography and Further Reading

Kudryavtseva, V M, ed., Zhidkostnikh Raketnikh Dvigatley, Visshaya Shkola, Moscow, 1993. ISBN: 5060025632. Russian-language textbook on rocket theory. More at amazon.com...

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