N1M 1965

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N1M 1965 - B

Part of N1 Block B

LOx/Kerosene propellant rocket stage. As per N1 improvement study, 1965. Further stretch of Block B and thrust increased again to 280 metric tons per engine.

Status: Study 1965. Thrust: 21,960.00 kN (4,936,800 lbf). Gross mass: 620,000 kg (1,360,000 lb). Unfuelled mass: 75,000 kg (165,000 lb). Specific impulse: 346 s. Burn time: 85 s. Height: 30.00 m (98.00 ft). Diameter: 6.80 m (22.30 ft). Span: 9.80 m (32.10 ft).

No Engines: 8.

Country: Russia. Engines: 11D52M. Launch Vehicles: N-IM 1965, N-IMV-III. Propellants: Lox/Kerosene.

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