This page no longer updated from 31 October 2001. Latest version can be found at N1 1962 - A

Gross Mass: 1,384,000 kg. Empty Mass: 117,000 kg. Thrust (vac): 4,020,000 kgf. Isp: 331 sec. Burn time: 103 sec. Propellants: Lox/Kerosene Isp(sl): 296 sec. Diameter: 10.0 m. Span: 17.0 m. Length: 30.0 m. Country: Russia. No Engines: 24. NK-15 Status: Design 1962. Comments: Includes 14,000 kg for Stage 1-2 interstage and payload fairing. Compared to total fuelled mass excludes 15,000 kg propellant expended in thrust build-up and boil-off prior to liftoff. Values as in draft project as defended on 2-16 July 1962.
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Last update 12 March 2001.
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© Mark Wade, 2001 .