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Saturn S-N C-3BN
Part of Nerva
Nuclear/LH2 propellant rocket stage. Nuclear upper stage considered in lieu of S-IVB in final Saturn C-3B study in November 1961.

Status: Study 1961. Thrust: 266.80 kN (59,979 lbf). Gross mass: 32,470 kg (71,580 lb). Unfuelled mass: 7,708 kg (16,993 lb). Specific impulse: 800 s. Burn time: 720 s. Height: 16.56 m (54.33 ft). Diameter: 10.06 m (33.00 ft). Span: 10.06 m (33.00 ft).



Family: Space Tugs. Country: USA. Engines: Nerva-1. Launch Vehicles: Saturn C-3BN. Propellants: Nuclear/LH2.

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