Saturn IC F-1 engine Credit - © Mark Wade Gross Mass: 2,286,217 kg (5,040,245 lb). Empty Mass: 135,218 kg (298,104 lb). Thrust (vac): 38,703.160 kN (8,700,816 lbf). Isp: 304 sec. Burn time: 161 sec. Propellants: Lox/Kerosene. Isp(sl): 265 sec. Diameter: 10.06 m (33.00 ft). Span: 19.00 m (62.00 ft). Length: 42.06 m (137.99 ft). Country: USA. No Engines: 5. Engine: F-1. Cost $ : 391.500 million. First Flight: 1967. Last Flight: 1973. No Launched: 13. Used on Launch Vehicles: Saturn INT-20. Saturn INT-21. Saturn MLV-V-4(S). Saturn Shuttle. Saturn V. Saturn V-A. Saturn V-Centaur.                   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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