Centaur D/E Centaur Credit - © Mark Wade Gross Mass: 16,258 kg (35,842 lb). Empty Mass: 2,631 kg (5,800 lb). Thrust (vac): 131.222 kN (29,500 lbf). Isp: 444 sec. Burn time: 470 sec. Propellants: Lox/LH2. Isp(sl): 0 sec. Diameter: 3.05 m (10.00 ft). Span: 3.05 m (10.00 ft). Length: 9.60 m (31.40 ft). Country: USA. No Engines: 2. Engine: RL-10A-3. Status: Study 1968. Cost $ : 20.300 million. First Flight: 1967. Last Flight: 1983. No Launched: 56. No Failed: 4. Used as: Atlas Centaur D; Titan 3E. Used on Launch Vehicles: Atlas Centaur SLV-3C. Atlas Centaur SLV-3D. Saturn IB-A. Saturn IB-CE. Saturn V-Centaur. Titan 3BAS2. Titan 3E. Titan 3L2. Titan 3L4.                   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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