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Saturn IB-A
Part of Saturn I
Saturn IB-A
Saturn IB-A
Credit: © Mark Wade
American orbital launch vehicle. Douglas Studies, 1965: S-IB with 225 k lbf H-1's; S-IVB stretched with 350,000 lbs propellants; Centaur third stage.

Status: Study 1965. Payload: 18,600 kg (41,000 lb). Thrust: 8,006.60 kN (1,799,955 lbf). Gross mass: 605,980 kg (1,335,950 lb). Height: 62.00 m (203.00 ft). Diameter: 6.61 m (21.68 ft). Apogee: 185 km (114 mi).

LEO Payload: 18,600 kg (41,000 lb) to a 185 km orbit at 28.00 degrees. Flyaway Unit Cost 1985$: 20.300 million.

Stage Data - Saturn IB-A



Family: orbital launch vehicle. People: von Braun. Country: USA. Engines: H-1c, RL-10A-3, J-2. Stages: Saturn IVB-A, Saturn S-IB-A, Centaur D/E.

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