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Atlas G/H/I
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Gross Mass: 142,536 kg (314,238 lb). Empty Mass: 4,236 kg (9,338 lb). Thrust (vac): 386.300 kN (86,844 lbf). Isp: 316 sec. Burn time: 266 sec. Propellants: Lox/Kerosene. Isp(sl): 220 sec. Diameter: 3.05 m (10.00 ft). Span: 4.90 m (16.00 ft). Length: 22.20 m (72.80 ft). Country: USA. No Engines: 1. Engine: LR-105-7. Status: Out of production. Cost $ : 50.000 million. First Flight: 1983. Last Flight: 1997. No Launched: 23. No Failed: 1.
Used on Launch Vehicles:
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© Mark Wade, 1997 - 2007 except where otherwise noted.
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