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Saturn IB-CE
Part of Saturn I
Saturn IB-CE
Saturn IB-CE
Credit: © Mark Wade
American orbital launch vehicle. Douglas Studies, 1965: Standard Saturn IB with Centaur upper stage.

Status: Study 1965. Payload: 22,000 kg (48,000 lb). Thrust: 7,295.10 kN (1,640,004 lbf). Gross mass: 610,110 kg (1,345,060 lb). Height: 62.00 m (203.00 ft). Diameter: 6.61 m (21.68 ft). Apogee: 185 km (114 mi).

LEO Payload: 22,000 kg (48,000 lb) to a 185 km orbit at 28.00 degrees. Payload: 5,590 kg (12,320 lb) to a translunar trajectory. Flyaway Unit Cost 1985$: 63.800 million.

Stage Data - Saturn IB-CE



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

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