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N1U 1965 - V
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Gross Mass: 193,000 kg (425,000 lb). Empty Mass: 15,000 kg (33,000 lb). Thrust (vac): 1,560.000 kN (350,700 lbf). Isp: 347 sec. Burn time: 380 sec. Propellants: Lox/Kerosene. Diameter: 4.80 m (15.70 ft). Span: 6.80 m (22.30 ft). Length: 12.00 m (39.00 ft). Country: Russia. No Engines: 4. Engine: NK-19. 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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