This page no longer updated from 31 October 2001. Latest version can be found at www.astronautix.com
Used on stages: RITA C. Used on launch vehicles: RITA C. Propellants: Nuclear/Lox/LH2 Thrust(vac): 2,460,250 kgf. Thrust(vac): 24,126.00 kN. Isp: 810 sec. Isp (sea level): 410 sec. Burn time: 285 sec. Chambers: 1. Country: USA. Status: Study 1963.
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Last update 12 March 2001.
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© Mark Wade, 2001 .