Atlas MA-3 Gross Mass: 3,174 kg (6,997 lb). Empty Mass: 3,174 kg (6,997 lb). Thrust (vac): 1,644.960 kN (369,802 lbf). Isp: 290 sec. Burn time: 120 sec. Propellants: Lox/Kerosene. Isp(sl): 256 sec. Diameter: 4.90 m (16.00 ft). Span: 4.90 m (16.00 ft). Length: 0.00 m ( ft). Country: USA. No Engines: 2. Engine: LR-89-5. First Flight: 1960. Last Flight: 1995. No Launched: 252. Used on Launch Vehicles: Atlas Centaur LV-3C. Atlas E. Atlas F. Atlas LV-3A / Agena B. SLV-3 Atlas. SLV-3 Atlas / Agena B. SLV-3 Atlas / Agena 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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