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Saturn S-IC-8
Part of Saturn IC Family
LOx/Kerosene propellant rocket stage. .

Status: Study 1960. Thrust: 61,925.00 kN (13,921,293 lbf). Gross mass: 3,627,500 kg (7,997,200 lb). Unfuelled mass: 181,400 kg (399,900 lb). Specific impulse: 304 s. Specific impulse sea level: 265 s. Burn time: 157 s. Height: 48.79 m (160.07 ft). Diameter: 12.19 m (39.99 ft). Span: 22.87 m (75.03 ft).

No Engines: 8.



Country: USA. Engines: F-1. Launch Vehicles: Saturn C-8. Propellants: Lox/Kerosene.

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