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N1 1964 - A
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Gross Mass: 1,942,000 kg (4,281,000 lb). Empty Mass: 192,000 kg (423,000 lb). Thrust (vac): 49,420.000 kN (11,110,050 lbf). Isp: 331 sec. Burn time: 113 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: Development ended 1964. As per draft project for N1-L3, 1964. Block A modified with six additional engines and propellant increased by 550 tonnes by using chilled propellants.
Used on Launch Vehicles:
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