This page no longer updated from 31 October 2001. Latest version can be found at www.astronautix.com
Used on stages: Saturn LCB-Lox/RP-1. Used on launch vehicles: Saturn LCB-Lox/RP-1. Propellants: Lox/Kerosene Thrust(vac): 2,070,700 kgf. Thrust(vac): 20,306.00 kN. Isp: 275 sec. Isp (sea level): 253 sec. Burn time: 163 sec. Chambers: 1. Country: USA. Status: Design concept 1960's.
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Last update 12 March 2001.
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© Mark Wade, 2001 .