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Saturn MS-II-3B
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Gross Mass: 643,200 kg (1,418,000 lb). Empty Mass: 53,500 kg (117,900 lb). Thrust (vac): 12,455.400 kN (2,800,085 lbf). Isp: 447 sec. Burn time: 204 sec. Propellants: Lox/LH2. Isp(sl): 200 sec. Diameter: 10.06 m (33.00 ft). Span: 10.06 m (33.00 ft). Length: 29.56 m (96.98 ft). Country: USA. No Engines: 5. Engine: Toroidal 400k. Status: Study 1967. S-II with 15.5 foot stretch, 1.29 million pounds propellant, 7 x 400,000 lb thrust toroidal engines.
Used on Launch Vehicles:
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© Mark Wade, 1997 - 2007 except where otherwise noted.
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