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Saturn MLV-V-4(S)
Part of Saturn V

S-1C details

S-1C details
Credit: © Mark Wade

American orbital launch vehicle. MSFC study, 1965. Saturn V core, strengthened but not stretched, with 4 Titan UA1205 strap-on solid rocket boosters.

Status: Study 1965. Payload: 118,000 kg (260,000 lb). Thrust: 54,911.50 kN (12,344,596 lbf). Gross mass: 3,947,350 kg (8,702,410 lb). Height: 102.00 m (334.00 ft). Diameter: 10.06 m (33.00 ft). Apogee: 185 km (114 mi).

LEO Payload: 118,000 kg (260,000 lb) to a 185 km orbit at 28.00 degrees. Payload: 52,900 kg (116,600 lb) to a translunar trajectory. Flyaway Unit Cost 1985$: 463.420 million.

Stage Data - Saturn MLV-V-4(S)



Family: orbital launch vehicle. People: von Braun. Country: USA. Engines: F-1. Stages: Saturn IC, Saturn MS-IVB-1, Saturn MS-II-4(S)B, UA1205.

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