Saturn S-IB-4 Gross Mass: 1,813,729 kg (3,998,587 lb). Empty Mass: 108,823 kg (239,913 lb). Thrust (vac): 30,962.526 kN (6,960,653 lbf). Isp: 304 sec. Burn time: 155 sec. Propellants: Lox/Kerosene. Isp(sl): 265 sec. Diameter: 10.06 m (33.00 ft). Span: 11.28 m (37.00 ft). Length: 28.96 m (95.01 ft). Country: USA. No Engines: 4. Engine: F-1. Status: Study 1960. Used on Launch Vehicles: Saturn C-4.                   Contact us with any corrections, additions, or comments. Conditions for use of drawings, pictures, or other materials from this site.. To contact astronauts or cosmonauts. © Mark Wade, 1997 - 2007 except where otherwise noted.

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