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Saturn S-1B-4 H-1
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Gross Mass: 444,700 kg (980,300 lb). Empty Mass: 37,600 kg (82,800 lb). Thrust (vac): 4,120.700 kN (926,370 lbf). Isp: 296 sec. Burn time: 282 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: 4. Engine: H-1b. Status: Study 1966. Chrysler Studies, 1966: S-1B with 4 H-1's for use with Titan UA1205 strap-ons
Used on Launch Vehicles:
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© Mark Wade, 1997 - 2007 except where otherwise noted.
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