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N1F 1965 - A
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Gross Mass: 1,940,000 kg (4,270,000 lb). Empty Mass: 200,000 kg (440,000 lb). Thrust (vac): 57,560.000 kN (12,940,000 lbf). Isp: 331 sec. Burn time: 100 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: 11D51F. Status: Study 1965. As per N1 improvement study, 1965. Block A engine thrust increased but little additional propellant.
Used on Launch Vehicles:
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