Saturn II Saturn II stage Credit - © Mark Wade Gross Mass: 490,778 kg (1,081,980 lb). Empty Mass: 39,048 kg (86,086 lb). Thrust (vac): 5,165.790 kN (1,161,316 lbf). Isp: 421 sec. Burn time: 390 sec. Propellants: Lox/LH2. Isp(sl): 200 sec. Diameter: 10.06 m (33.00 ft). Span: 10.06 m (33.00 ft). Length: 24.84 m (81.49 ft). Country: USA. No Engines: 5. Engine: J-2. Cost $ : 290.000 million. First Flight: 1967. Last Flight: 1973. No Launched: 13. Used on Launch Vehicles: Saturn INT-18. Saturn INT-21. Saturn V. Saturn V-Centaur. Saturn V-D.                   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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