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N1 Nuclear V stage
Part of N1 Nuclear V Family
Nuclear/LH2 propellant rocket stage. N1 nuclear upper stage study, 1963. Figures calculated based on given total stage thrust, specific impulse, engine mass.

AKA: N1 Nuclear V. Status: Study 1963. Thrust: 14,700.00 kN (3,304,600 lbf). Gross mass: 1,500,000 kg (3,300,000 lb). Unfuelled mass: 500,000 kg (1,100,000 lb). Specific impulse: 900 s. Burn time: 590 s. Height: 100.00 m (320.00 ft). Diameter: 17.00 m (55.00 ft). Span: 17.00 m (55.00 ft).

No Engines: 20.



Country: Russia. Engines: YaRD Type V. Launch Vehicles: N1 Nuclear V. Propellants: Nuclear/LH2.

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