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Saturn INT-17
Part of Saturn V
Saturn 1B/120-7 seg
Saturn 1B/120-7 seg
Saturn 1B with 120 inch 7 segment strap on
Credit: © Mark Wade
North American study, 1966. Saturn variant with a modified S-II first stage with seven high-performance HG-3 engines; S-IVB second stage. Poor performance and cost-effectiveness and not studied further.

Status: Study 1966. Payload: 42,000 kg (92,000 lb). Thrust: 5,936.01 kN (1,334,468 lbf). Gross mass: 504,400 kg (1,112,000 lb). Height: 51.00 m (167.00 ft). Diameter: 10.06 m (33.00 ft). Apogee: 185 km (114 mi).

LEO Payload: 42,000 kg (92,000 lb) to a 185 km orbit at 28.00 degrees.

Stage Data - Saturn INT-17



Family: orbital launch vehicle. People: von Braun. Country: USA. Engines: HG-3-SL. Stages: Saturn II-INT-17, Saturn IVB (S-IB).

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