This page no longer updated from 31 October 2001. Latest version can be found at Saturn S-1B-4 H-1

Gross Mass: 444,700 kg. Empty Mass: 37,600 kg. Thrust (vac): 420,200 kgf. Isp: 296 sec. Burn time: 282 sec. Propellants: Lox/Kerosene Isp(sl): 262 sec. Diameter: 6.5 m. Span: 6.5 m. Length: 24.5 m. Country: USA. No Engines: 4. H-1b Status: Study 1966. Comments: Chrysler Studies, 1966: S-1B with 4 H-1's for use with Titan UA1205 strap-ons.
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Last update 12 March 2001.
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© Mark Wade, 2001 .