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Saturn MS-IC-1A
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Gross Mass: 2,694,700 kg (5,940,700 lb). Empty Mass: 160,600 kg (354,000 lb). Thrust (vac): 46,443.300 kN (10,440,869 lbf). Isp: 304 sec. Burn time: 160 sec. Propellants: Lox/Kerosene. Isp(sl): 265 sec. Diameter: 10.06 m (33.00 ft). Span: 19.01 m (62.36 ft). Length: 48.16 m (158.00 ft). Country: USA. No Engines: 6. Engine: F-1. Status: Study 1965. Basic Saturn IC stretched 240 inches with 6 F-1 engines.
Used on Launch Vehicles:
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© Mark Wade, 1997 - 2007 except where otherwise noted.
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