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Saturn MS-II-1
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Gross Mass: 521,447 kg (1,149,593 lb). Empty Mass: 49,877 kg (109,959 lb). Thrust (vac): 5,165.790 kN (1,161,316 lbf). Isp: 425 sec. Burn time: 361 sec. Propellants: Lox/LH2. Isp(sl): 306 sec. Diameter: 10.06 m (33.00 ft). Span: 10.06 m (33.00 ft). Length: 25.88 m (84.90 ft). Country: USA. No Engines: 5. Engine: J-2. Status: Study 1965. Basic Saturn II with 41 inch stretch of hydrogen tank.
Used on Launch Vehicles:
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© Mark Wade, 1997 - 2007 except where otherwise noted.
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