This page no longer updated from 31 October 2001. Latest version can be found at www.astronautix.com
Used on stages: Nova MM T10RR-2-2. Used on launch vehicles: Nova MM T10RR-2. Propellants: Lox/LH2 Thrust(vac): 2,041,000 kgf. Thrust(vac): 20,015.00 kN. Isp: 455 sec. Burn time: 408 sec. Chambers: 1. Country: USA. Status: Study 1963. Comments: Operational date would have been December 1976. Engines for recoverable stage.
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Last update 12 March 2001.
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© Mark Wade, 2001 .