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Saturn INT-11
Part of Saturn I
Saturn IB-INT-11
Saturn IB-INT-11
Credit: © Mark Wade
American orbital launch vehicle. Chrysler Studies, 1966: S-IB with 4 Titan UA1205 with standard S-IB stage, S-IVB stage, or 4 Titan UA1207 strap-ons with 20-foot stretched S-IB stage, S-IVB stage. S-IB ignition at altitude.

Status: Study 1966. Payload: 48,000 kg (105,000 lb). Thrust: 25,642.10 kN (5,764,573 lbf). Gross mass: 1,959,670 kg (4,320,330 lb). Height: 58.00 m (190.00 ft). Diameter: 6.61 m (21.68 ft). Apogee: 169 km (105 mi).

LEO Payload: 48,000 kg (105,000 lb) to a 169 km orbit at 28.00 degrees. Flyaway Unit Cost 1985$: 97.440 million.

Stage Data - Saturn INT-11



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

Saturn 1B/4 SRBsSaturn 1B/4 SRBs
Saturn 1B with 4 solids replacing S-1B
Credit: © Mark Wade



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