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Atlas II
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Gross Mass: 161,995 kg (357,137 lb). Empty Mass: 6,095 kg (13,437 lb). Thrust (vac): 386.300 kN (86,844 lbf). Isp: 316 sec. Burn time: 283 sec. Propellants: Lox/Kerosene. Isp(sl): 220 sec. Diameter: 3.05 m (10.00 ft). Span: 3.05 m (10.00 ft). Length: 24.90 m (81.60 ft). Country: USA. No Engines: 1. Engine: RS-56-OSA. Status: Out of production. Cost $ : 55.000 million. First Flight: 1991. Last Flight: 1998. No Launched: 10.
Used on Launch Vehicles:
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© Mark Wade, 1997 - 2007 except where otherwise noted.
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