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Saturn S-II-8
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Gross Mass: 770,835 kg (1,699,400 lb). Empty Mass: 63,480 kg (139,940 lb). Thrust (vac): 8,265.260 kN (1,858,104 lbf). Isp: 425 sec. Burn time: 338 sec. Propellants: Lox/LH2. Isp(sl): 306 sec. Diameter: 10.06 m (33.00 ft). Span: 10.06 m (33.00 ft). Length: 42.68 m (140.02 ft). Country: USA. No Engines: 8. Engine: J-2. Status: Study 1960.
Used on Launch Vehicles:
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© Mark Wade, 1997 - 2007 except where otherwise noted.
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