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Saturn MS-IC-23(L)
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Gross Mass: 2,694,000 kg (5,939,000 lb). Empty Mass: 169,000 kg (372,000 lb). Thrust (vac): 38,703.160 kN (8,700,816 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: 48.15 m (157.97 ft). Country: USA. No Engines: 5. Engine: F-1. Status: Study 1967. Basic Saturn IC stretched 240 inches with standard F-1 engines.
Used on Launch Vehicles:
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© Mark Wade, 1997 - 2007 except where otherwise noted.
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