Saturn MS-IC-4(S)B

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Saturn MS-IC-4(S)B

Part of Saturn IC

LOx/Kerosene propellant rocket stage. S-IC with 336 inch stretch, 6,000,0000 lbs propellant, structural strength increased from 56% to 65% depending on station, resulting in 13.9% increase in empty weight.

Status: Study 1966. Thrust: 38,717.60 kN (8,704,063 lbf). Gross mass: 2,875,500 kg (6,339,300 lb). Unfuelled mass: 154,000 kg (339,000 lb). Specific impulse: 304 s. Specific impulse sea level: 265 s. Burn time: 206 s. Height: 50.58 m (165.94 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 MLV-V-4(S)-A, Saturn V-ELV. Propellants: Lox/Kerosene.

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