Saturn S-N C-5N

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Saturn S-N C-5N

Part of Nerva

Nuclear/LH2 propellant rocket stage. Nuclear upper stage considered in lieu of S-IVB in final Saturn C-5 study in November 1961.

Status: Study 1961. Thrust: 266.80 kN (59,979 lbf). Gross mass: 53,694 kg (118,375 lb). Unfuelled mass: 10,429 kg (22,992 lb). Specific impulse: 800 s. Burn time: 1,250 s. Height: 19.30 m (63.30 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-5N. Propellants: Nuclear/LH2.

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