N1F 1965

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N1F 1965 - B

Part of N1 Block B

LOx/Kerosene propellant rocket stage. As per N1 improvement study, 1965. Engine thrust increased from 150 t each to 200 t and stretched propellant tanks.

Status: Study 1965. Thrust: 15,600.00 kN (3,507,000 lbf). Gross mass: 590,000 kg (1,300,000 lb). Unfuelled mass: 60,000 kg (132,000 lb). Specific impulse: 346 s. Burn time: 115 s. Height: 26.00 m (85.00 ft). Diameter: 6.80 m (22.30 ft). Span: 9.80 m (32.10 ft).

No Engines: 8.

Country: Russia. Engines: 11D52F. Launch Vehicles: N-IF 1965, N-IFV-III. Propellants: Lox/Kerosene.

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