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N1F 1965 - A
Part of N1 Block A Family
LOx/Kerosene propellant rocket stage. As per N1 improvement study, 1965. Block A engine thrust increased but little additional propellant.

Status: Study 1965. Thrust: 57,560.00 kN (12,940,000 lbf). Gross mass: 1,940,000 kg (4,270,000 lb). Unfuelled mass: 200,000 kg (440,000 lb). Specific impulse: 331 s. Specific impulse sea level: 296 s. Burn time: 100 s. Height: 30.00 m (98.00 ft). Diameter: 10.00 m (32.00 ft). Span: 17.00 m (55.00 ft).

No Engines: 30.



Country: Russia. Engines: 11D51F. Launch Vehicles: N-IF 1965, N-IFV-III, N-IFV-II-III. Propellants: Lox/Kerosene.

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