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N1 Nuclear V-Bioshield
Part of N1 Nuclear V
Nuclear/LH2 propellant rocket stage. N1 nuclear upper stage study, 1963. Figures calculated based on given total stage thrust, specific impulse, engine mass.
Status: Study 1963. Thrust: 19,600.00 kN (4,406,200 lbf). Gross mass: 2,000,000 kg (4,400,000 lb). Unfuelled mass: 650,000 kg (1,430,000 lb). Specific impulse: 900 s. Burn time: 600 s. Height: 130.00 m (420.00 ft). Diameter: 17.00 m (55.00 ft). Span: 17.00 m (55.00 ft).
No Engines: 20.
Country:
Russia.
Engines:
YaRD Type V-B.
Launch Vehicles:
N1 Nuclear V-B.
Propellants:
Nuclear/LH2.
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