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Saturn INT-13
Part of Saturn I
American orbital launch vehicle. Chrysler Studies, 1966: S-IB with 2 Titan UA1205 with standard length S-IB stage, S-IVB stage, or 2 Titan UA1207 strap-ons with 20-foot stretched S-IB stage, S-IVB stage. S-IB ignition at sea level at same time as strap-ons.

Status: Study 1966. Payload: 36,590 kg (80,660 lb). Thrust: 20,116.10 kN (4,522,279 lbf). Gross mass: 1,307,320 kg (2,882,140 lb). Height: 58.00 m (190.00 ft). Diameter: 6.61 m (21.68 ft). Apogee: 169 km (105 mi).

LEO Payload: 36,590 kg (80,660 lb) to a 169 km orbit at 28.00 degrees. Flyaway Unit Cost 1985$: 48.720 million.

Stage Data - Saturn INT-13



Family: orbital launch vehicle. People: von Braun. Country: USA. Engines: H-1b. Stages: Saturn IB-11, Saturn IVB (S-IB), UA1207.

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