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Saturn INT-14
Part of Saturn I
Saturn IB-INT-14
Saturn IB-INT-14
Credit: © Mark Wade
American orbital launch vehicle. Chrysler Studies, 1966: S-IB with 4 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: 23,180 kg (51,100 lb). Thrust: 9,886.40 kN (2,222,551 lbf). Gross mass: 750,570 kg (1,654,720 lb). Height: 58.00 m (190.00 ft). Diameter: 6.61 m (21.68 ft). Apogee: 169 km (105 mi).

LEO Payload: 23,180 kg (51,100 lb) to a 169 km orbit at 28.00 degrees.

Stage Data - Saturn INT-14



Family: orbital launch vehicle. People: von Braun. Country: USA. Engines: H-1b. Stages: Saturn IB-11, Saturn IVB (S-IB), M55/TX-55/Tu-122.
Photo Gallery

Saturn 1B/MM SRBSaturn 1B/MM SRB
Saturn 1B with Minuteman strapons
Credit: © Mark Wade



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