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Saturn S-II-4
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Gross Mass: 294,731 kg (649,770 lb). Empty Mass: 24,938 kg (54,978 lb). Thrust (vac): 3,557.313 kN (799,716 lbf). Isp: 420 sec. Burn time: 296 sec. Propellants: Lox/LH2. Isp(sl): 300 sec. Diameter: 10.06 m (33.00 ft). Span: 10.06 m (33.00 ft). Length: 16.76 m (54.98 ft). Country: USA. No Engines: 4. 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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