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N1F Block A
Part of N1 Block A Family
LOx/Kerosene propellant rocket stage. Includes 14,000 kg for Stage 1-2 interstage.

Status: Development ended 1974. Thrust: 49,675.50 kN (11,167,497 lbf). Gross mass: 2,070,000 kg (4,560,000 lb). Unfuelled mass: 126,230 kg (278,280 lb). Specific impulse: 331 s. Specific impulse sea level: 297 s. Burn time: 125 s. Height: 30.00 m (98.00 ft). Diameter: 10.00 m (32.00 ft). Span: 15.60 m (51.10 ft).

No Engines: 30.



Country: Russia. Engines: 11D121, NK-33. Launch Vehicles: N1F, N1F Sr, N1F-L3M. Propellants: Lox/Kerosene.

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