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Saturn INT-16
Part of Saturn I
Saturn IB-INT-16
Saturn IB-INT-16
Credit: © Mark Wade
American orbital launch vehicle. UA Studies, 1966: S-IVB upper stage with from 2 to 5 Titan UA1205, 1206, or 1207 motors as first stage, clustered around from 1 to 3 of the same motors as a second stage. S-IVB upper stage.

Status: Study 1966. Payload: 28,000 kg (61,000 lb). Thrust: 26,466.90 kN (5,949,996 lbf). Gross mass: 1,283,570 kg (2,829,780 lb). Height: 52.00 m (170.00 ft). Diameter: 6.61 m (21.68 ft). Apogee: 185 km (114 mi).

LEO Payload: 28,000 kg (61,000 lb) to a 185 km orbit at 28.00 degrees. Flyaway Unit Cost 1985$: 89.900 million.

Stage Data - Saturn INT-16



Family: orbital launch vehicle. People: von Braun. Country: USA. Stages: Saturn IVB (S-IB), UA1205.

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