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Saturn INT-18
Part of Saturn V
Saturn 2SL/120
Saturn 2SL/120" SRB
Saturn 2SL 120 inch strapons
Credit: © Mark Wade
North American study, 1966. Saturn variant with Titan UA1205 or 1207 motors as boosters, Saturn II stage as core, and Saturn IVB upper stage. Various combinations of numbers of strap-ons, propellant loading of the two core stages, and sea-level versus altitude ignition were studied.

Status: Study 1966. Payload: 66,590 kg (146,800 lb). Thrust: 25,642.10 kN (5,764,573 lbf). Gross mass: 1,966,810 kg (4,336,070 lb). Height: 51.00 m (167.00 ft). Diameter: 10.06 m (33.00 ft). Apogee: 185 km (114 mi).

Liftoff Mass - kgStrapon Motor TypeNumber of StraponsS-II Propellant - kgS-IVB Propellant - kgPayload - kg
1,132,000Titan UA12044215,40080,30021,300
1,132,000Titan UA12044215,40078,50023,100
1,030,400Titan UA12072254,00080,70027,400
1,132,400Titan UA12072349,20079,80035,400
1,083,000Titan UA12052431,60077,40040,500
1,570,500Titan UA12054440,40074,40051,700
1,895,200Titan UA12074446,70075,70066,400
1,476,200Titan UA12054446,700No S-IVB39,000
1,779,600Titan UA12074446,700No S-IVB44,000

LEO Payload: 66,590 kg (146,800 lb) to a 185 km orbit at 28.00 degrees. Flyaway Unit Cost 1985$: 387.440 million.

Stage Data - Saturn INT-18



Family: orbital launch vehicle. People: von Braun. Country: USA. Stages: Saturn II, Saturn IVB (S-IB), UA1207.
Photo Gallery

Saturn MLV 2-120-7Saturn MLV 2-120-7
Credit: © Mark Wade


Saturn 2-120-5Saturn 2-120-5
Credit: © Mark Wade


Saturn 2-120-4Saturn 2-120-4
Credit: © Mark Wade



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