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Saturn MLV 5-23L-0
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Gross Mass: 1,180,000 kg (2,600,000 lb). Empty Mass: 80,000 kg (176,000 lb). Thrust (vac): 15,484.000 kN (3,480,941 lbf). Isp: 304 sec. Burn time: 200 sec. Propellants: Lox/Kerosene. Isp(sl): 265 sec. Diameter: 6.61 m (21.68 ft). Span: 6.61 m (21.68 ft). Length: 51.00 m (167.00 ft). Country: USA. No Engines: 2. Engine: F-1. Status: Study 1966. Liquid strap-on booster studied for improved Saturn V.
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© Mark Wade, 1997 - 2007 except where otherwise noted.
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