Saturn S-IC-8 Gross Mass: 3,627,500 kg (7,997,200 lb). Empty Mass: 181,400 kg (399,900 lb). Thrust (vac): 61,925.000 kN (13,921,293 lbf). Isp: 304 sec. Burn time: 157 sec. Propellants: Lox/Kerosene. Isp(sl): 265 sec. Diameter: 12.19 m (39.99 ft). Span: 22.87 m (75.03 ft). Length: 48.79 m (160.07 ft). Country: USA. No Engines: 8. Engine: F-1. Status: Study 1960. Used on Launch Vehicles: Saturn C-8.                   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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