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Atlas MA-2
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Gross Mass: 3,050 kg (6,720 lb). Empty Mass: 3,050 kg (6,720 lb). Thrust (vac): 1,517.422 kN (341,130 lbf). Isp: 282 sec. Burn time: 135 sec. Propellants: Lox/Kerosene. Isp(sl): 248 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: XLR-89-5. First Flight: 1958. Last Flight: 1967. No Launched: 160.
Used on Launch Vehicles:
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© Mark Wade, 1997 - 2007 except where otherwise noted.
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