This page no longer updated from 31 October 2001. Latest version can be found at www.astronautix.com
Used on stages: Pegasus VTOVL. Used on launch vehicles: Pegasus VTOVL. Propellants: Lox/LH2 Thrust(vac): 2,440,000 kgf. Thrust(vac): 23,928.00 kN. Isp: 459 sec. Isp (sea level): 359 sec. Burn time: 232 sec. Chambers: 1. Country: USA. Status: Study 1966.
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Last update 12 March 2001.
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© Mark Wade, 2001 .