Saturn IB-C (original) (raw)


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Saturn IB-C


Part of Saturn I


Saturn IB-C
Saturn IB-C
Credit: © Mark Wade

American orbital launch vehicle. Douglas Studies, 1965: 4 Minuteman strap-ons; standard S-IB, S-IVB stages.

Status: Study 1965. Payload: 20,400 kg (44,900 lb). Thrust: 9,886.40 kN (2,222,551 lbf). Gross mass: 689,930 kg (1,521,030 lb). Height: 51.00 m (167.00 ft). Diameter: 6.61 m (21.68 ft). Apogee: 185 km (114 mi).

LEO Payload: 20,400 kg (44,900 lb) to a 185 km orbit at 28.00 degrees. Flyaway Unit Cost 1985$: 43.500 million.

Stage Data - Saturn IB-C



Family: orbital launch vehicle. People: von Braun. Country: USA. Engines: H-1b. Stages: Saturn IB stage, Saturn IVB (S-IB), M55/TX-55/Tu-122.



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