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Gross Mass: 506,000 kg.
Empty Mass: 50,000 kg. Thrust (vac): 1,400,000 kgf. Isp: 346 sec. Burn time: 106 sec. Propellants: Lox/Kerosene Diameter: 6.8 m. Span: 9.8 m. Length: 20.0 m. Country: Russia. No Engines: 8. NK-15V Status: Design 1964. Comments: As per draft project for N1-L3, 1964. Specific impulse estimate down one second from 1962 draft project. Thrust said to be increased 2% but not reflected in figures given.
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Last update 12 March 2001.
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© Mark Wade, 2001 .