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Saturn MS-IC/260
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Gross Mass: 2,721,600 kg (6,000,100 lb). Empty Mass: 181,400 kg (399,900 lb). Thrust (vac): 38,717.600 kN (8,704,063 lbf). Isp: 304 sec. Burn time: 192 sec. Propellants: Lox/Kerosene. Isp(sl): 265 sec. Diameter: 10.06 m (33.00 ft). Span: 19.00 m (62.00 ft). Length: 42.05 m (137.95 ft). Country: USA. No Engines: 5. Engine: F-1. Status: Study 1967. Standard length S-IC but with feed of propellant from fuel and propellant tanks housed above strap-on solid rocket motors
Used on Launch Vehicles:
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© Mark Wade, 1997 - 2007 except where otherwise noted.
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