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N1 Nuclear A stage
Part of N1 Nuclear A 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 A. Status: Study 1963. Thrust: 6,860.00 kN (1,542,180 lbf). Gross mass: 700,000 kg (1,540,000 lb). Unfuelled mass: 250,000 kg (550,000 lb). Specific impulse: 900 s. Burn time: 570 s. Height: 90.00 m (295.00 ft). Diameter: 12.00 m (39.00 ft). Span: 12.00 m (39.00 ft).

No Engines: 40.



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

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