N1M 1965

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N1M 1965 - V

Part of N1 Block V

LOx/Kerosene propellant rocket stage. As per N1 improvement study, 1965. Further stretch of Block V.

Status: Study 1965. Thrust: 2,940.00 kN (660,930 lbf). Gross mass: 355,000 kg (782,000 lb). Unfuelled mass: 20,000 kg (44,000 lb). Specific impulse: 347 s. Burn time: 380 s. Height: 20.00 m (65.00 ft). Diameter: 4.80 m (15.70 ft). Span: 6.80 m (22.30 ft).

No Engines: 4.

Country: Russia. Engines: 11D53M. Launch Vehicles: N-IM 1965. Propellants: Lox/Kerosene.

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