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Saturn IC-Flat Bulkhead
Part of Saturn IC Family
LOx/Kerosene propellant rocket stage. Standard S-IC but with reduced length and structural weight through use of 'flat' bulkheads consisting of multiple conical sections.

Status: Study MSFC 1965. Thrust: 38,717.60 kN (8,704,063 lbf). Gross mass: 2,278,800 kg (5,023,800 lb). Unfuelled mass: 127,000 kg (279,000 lb). Specific impulse: 304 s. Specific impulse sea level: 265 s. Burn time: 161 s. Height: 36.55 m (119.91 ft). Diameter: 10.06 m (33.00 ft). Span: 19.00 m (62.00 ft).

No Engines: 5.



Country: USA. Engines: F-1. Propellants: Lox/Kerosene.

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