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Saturn INT-15
Part of Saturn I
Saturn 1B/120-5 seg
Saturn 1B/120-5 seg
Saturn 1B with 120 inch 5 segment strap on
Credit: © Mark Wade
American orbital launch vehicle. Chrysler Studies, 1966: S-IB with 8 Minuteman motors as strap-ons, with no, 10, or 20-foot stretch S-IB stages, S-IVB stage. S-IB ignition at sea level at same time as strap-ons.

Status: Study 1966. Payload: 26,000 kg (57,000 lb). Thrust: 12,477.80 kN (2,805,121 lbf). Gross mass: 824,100 kg (1,816,800 lb). Height: 54.00 m (177.00 ft). Diameter: 6.61 m (21.68 ft). Apogee: 169 km (105 mi).

LEO Payload: 26,000 kg (57,000 lb) to a 169 km orbit at 28.00 degrees.

Stage Data - Saturn INT-15



Family: orbital launch vehicle. People: von Braun. Country: USA. Engines: H-1b. Stages: Saturn IB-15, Saturn IVB (S-IB), M55/TX-55/Tu-122.

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