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Used on stages: Nova MM 34-0, Nova MM 34-1. Used on launch vehicles: Nova MM 34. Propellants: Lox/LH2 Thrust(vac): 12,517,000 kgf. Thrust(vac): 122,748.00 kN. Isp: 439 sec. Isp (sea level): 382 sec. Burn time: 388 sec. Chambers: 1. Country: USA. Status: Study 1963. Comments: Operational date would have been June 1976. Used in booster stage (engines only).
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Last update 12 March 2001.
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© Mark Wade, 2001 .