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N1 1964 - B
Part of N1 Block B Family
LOx/Kerosene propellant rocket stage. Second stage of the N1 superbooster. As per draft project for N1-L3, 1964. Specific impulse estimate down one second from 1962 draft project. Thrust said to be increased 2% but not reflected in figures given.

Status: Development ended 1964. Thrust: 13,700.00 kN (3,079,800 lbf). Gross mass: 506,000 kg (1,115,000 lb). Unfuelled mass: 50,000 kg (110,000 lb). Specific impulse: 346 s. Burn time: 106 s. Height: 20.00 m (65.00 ft). Diameter: 6.80 m (22.30 ft). Span: 9.80 m (32.10 ft).

No Engines: 8.



Country: Russia. Engines: NK-15V. Launch Vehicles: N1 1964. Propellants: Lox/Kerosene.

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