This page no longer updated from 31 October 2001. Latest version can be found at www.astronautix.com

astronautix.com 5 mlbf RP-4


Used on stages: Nova DAC-1. Used on launch vehicles: Nova-1 DAC. Propellants: Lox/Kerosene Thrust(vac): 2,494,250 kgf. Thrust(vac): 24,459.00 kN. Isp: 299 sec. Isp (sea level): 260 sec. Burn time: 118 sec. Chambers: 1. Country: USA. Status: Study 1963. Comments: Operational date would have been July 1977. Recoverable stage. 10% plug nozzle.
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Last update 12 March 2001.
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© Mark Wade, 2001 .