Atlas MA-5A Gross Mass: 4,187 kg (9,230 lb). Empty Mass: 4,187 kg (9,230 lb). Thrust (vac): 2,093.700 kN (470,682 lbf). Isp: 299 sec. Burn time: 172 sec. Propellants: Lox/Kerosene. Isp(sl): 263 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: RS-56-OBA. Status: Out of production. First Flight: 1991. Last Flight: 2002. No Launched: 33. Used on Launch Vehicles: Atlas II. Atlas IIA.                   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.

Encyclopedia Astronautica topic index 0 - A - B - C - D - E - F - G - H - I - J - K - L - M - N - O - P - Q - Ra - Re - Sa - Sf - Sp - T - U - V - W - X - Y - Z Enter your search terms   Web www.astronautix.com Submit search form