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N1U 1965 - A
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Gross Mass: 1,934,000 kg (4,263,000 lb). Empty Mass: 195,000 kg (429,000 lb). Thrust (vac): 49,420.000 kN (11,110,050 lbf). Isp: 331 sec. Burn time: 110 sec. Propellants: Lox/Kerosene. Isp(sl): 296 sec. Diameter: 10.00 m (32.00 ft). Span: 17.00 m (55.00 ft). Length: 30.00 m (98.00 ft). Country: Russia. No Engines: 30. Engine: NK-15. Status: Study 1965. As per N1 improvement study, 1965. Primarily improved reliability and produceability compared to first model.
Used on Launch Vehicles:
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© Mark Wade, 1997 - 2007 except where otherwise noted.
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