This page no longer updated from 31 October 2001. Latest version can be found at www.astronautix.com
Used on stages: Nova MM 24G-1, Nova MM 24G-2, Nova MM 33-1. Used on launch vehicles: Nova MM 24G, Nova MM 33. Propellants: Lox/LH2 Thrust(vac): 666,541 kgf. Thrust(vac): 6,536.00 kN. Isp: 451 sec. Isp (sea level): 379 sec. Burn time: 386 sec. Chambers: 1. Country: USA. Status: Study 1963. Comments: Operational date would have been December 1974.
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Last update 12 March 2001.
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© Mark Wade, 2001 .