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Saturn INT-05A
Part of Saturn I
Saturn IB-INT-5A
Saturn IB-INT-5A
Credit: © Mark Wade
American orbital launch vehicle. UA Study, 1965: Full length 260 inch solid motor with S-IVB upper stage.

Status: Study 1965. Payload: 43,034 kg (94,873 lb). Thrust: 32,027.10 kN (7,199,979 lbf). Gross mass: 1,818,800 kg (4,009,700 lb). Height: 58.00 m (190.00 ft). Diameter: 6.61 m (21.68 ft). Apogee: 185 km (114 mi).

LEO Payload: 43,034 kg (94,873 lb) to a 185 km orbit at 28.00 degrees. Flyaway Unit Cost 1985$: 111.650 million.

Stage Data - Saturn INT-05A



Family: orbital launch vehicle. People: von Braun. Country: USA. Stages: AJ-260-1/3, AJ-260X, Saturn IVB (S-IB).
Photo Gallery

Saturn IB-INT-5BSaturn IB-INT-5B
Credit: © Mark Wade



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