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Saturn S-IB-A
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Gross Mass: 448,600 kg (988,900 lb). Empty Mass: 41,600 kg (91,700 lb). Thrust (vac): 9,045.600 kN (2,033,532 lbf). Isp: 296 sec. Burn time: 128 sec. Propellants: Lox/Kerosene. Isp(sl): 262 sec. Diameter: 6.52 m (21.39 ft). Span: 6.52 m (21.39 ft). Length: 24.48 m (80.31 ft). Country: USA. No Engines: 8. Engine: H-1c. Status: Study 1965. Douglas Studies, 1965: S-1B with 225 k lbf H-1's
Used on Launch Vehicles:
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© Mark Wade, 1997 - 2007 except where otherwise noted.
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