This page no longer updated from 31 October 2001. Latest version can be found at www.astronautix.com
Used on stages: Saturn LCB-Storable-250. Used on launch vehicles: Saturn LCB-Storable-250. Propellants: N2O4/UDMH Thrust(vac): 2,165,100 kgf. Thrust(vac): 21,232.00 kN. Isp: 267 sec. Isp (sea level): 245 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 .