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Atlas MA-5
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Gross Mass: 3,646 kg (8,038 lb). Empty Mass: 3,646 kg (8,038 lb). Thrust (vac): 1,896.010 kN (426,240 lbf). Isp: 294 sec. Burn time: 174 sec. Propellants: Lox/Kerosene. Isp(sl): 259 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-89-7. Status: Out of production. First Flight: 1963. Last Flight: 1997. No Launched: 99.
Used on Launch Vehicles:
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© Mark Wade, 1997 - 2007 except where otherwise noted.
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