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Saturn V-C
Part of Saturn V
American orbital launch vehicle. MSFC study, 1968. S-ID stage-and-a-half first stage and Saturn IVB second stage. Centaur available as third stage for deep space missions. 30% performance improvement over Saturn V-A/Saturn INT-20 with standard Saturn IC first stage.

Status: Study 1968. Payload: 81,600 kg (179,800 lb). Thrust: 33,737.70 kN (7,584,537 lbf). Gross mass: 2,504,020 kg (5,520,410 lb). Height: 72.00 m (236.00 ft). Diameter: 10.06 m (33.00 ft). Apogee: 185 km (114 mi).

LEO Payload: 81,600 kg (179,800 lb) to a 185 km orbit at 28.00 degrees. Payload: 20,400 kg (44,900 lb) to a translunar trajectory.

Stage Data - Saturn V-C



Family: orbital launch vehicle. People: von Braun. Country: USA. Stages: Saturn IVB (S-V), Saturn S-ID Booster, Saturn S-ID Sustainer.

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