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Saturn IB-B
Part of Saturn I
Saturn IB-B
Saturn IB-B
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 and HG-3 high performance engine.

Status: Study 1965. Payload: 22,700 kg (50,000 lb). Thrust: 8,006.60 kN (1,799,955 lbf). Gross mass: 652,440 kg (1,438,380 lb). Height: 57.00 m (187.00 ft). Diameter: 6.61 m (21.68 ft). Apogee: 185 km (114 mi).

LEO Payload: 22,700 kg (50,000 lb) to a 185 km orbit at 28.00 degrees.

Stage Data - Saturn IB-B



Family: orbital launch vehicle. People: von Braun. Country: USA. Engines: H-1c, HG-3. Stages: Saturn MS-IVB-2, Saturn S-IB-A.

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