This page no longer updated from 31 October 2001. Latest version can be found at www.astronautix.com
Used on stages: Saturn MS-II-3B, Saturn MS-IVB-3B. Used on launch vehicles: Saturn V-3B. Propellants: Lox/LH2 Thrust(vac): 181,400 kgf. Thrust(vac): 1,778.00 kN. Isp: 447 sec. Isp (sea level): 200 sec. Burn time: 385 sec. Chambers: 1. Country: USA. Status: Design concept 1990's.
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Last update 12 March 2001.
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© Mark Wade, 2001 .