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N1 1964 - V
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Gross Mass: 193,000 kg (425,000 lb). Empty Mass: 16,000 kg (35,000 lb). Thrust (vac): 1,560.000 kN (350,700 lbf). Isp: 347 sec. Burn time: 368 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: Development ended 1964. As per draft project for N1-L3, 1964. Thrust said to be increased 2% but not reflected in figures given.
Used on Launch Vehicles:
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