Saturn MS-IC/260

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Saturn MS-IC/260

Part of Saturn IC

LOx/Kerosene propellant rocket stage. Standard length S-IC but with feed of propellant from fuel and propellant tanks housed above strap-on solid rocket motors.

Status: Study 1967. Thrust: 38,717.60 kN (8,704,063 lbf). Gross mass: 2,721,600 kg (6,000,100 lb). Unfuelled mass: 181,400 kg (399,900 lb). Specific impulse: 304 s. Specific impulse sea level: 265 s. Burn time: 192 s. Height: 42.05 m (137.95 ft). Diameter: 10.06 m (33.00 ft). Span: 19.00 m (62.00 ft).

No Engines: 5.

Country: USA. Engines: F-1. Launch Vehicles: Saturn V/4-260. Propellants: Lox/Kerosene.

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