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Saturn S-II-8
Part of Saturn II Family
LOx/LH2 propellant rocket stage. Version for Saturn C-8.

Status: Study 1960. Thrust: 8,265.26 kN (1,858,104 lbf). Gross mass: 770,835 kg (1,699,400 lb). Unfuelled mass: 63,480 kg (139,940 lb). Specific impulse: 425 s. Specific impulse sea level: 306 s. Burn time: 338 s. Height: 42.68 m (140.02 ft). Diameter: 10.06 m (33.00 ft). Span: 10.06 m (33.00 ft).

No Engines: 8.



Country: USA. Engines: J-2. Launch Vehicles: Saturn C-8. Propellants: Lox/LH2.

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