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Atlas Centaur SLV-3C/D
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Gross Mass: 128,500 kg (283,200 lb). Empty Mass: 4,000 kg (8,800 lb). Thrust (vac): 386.300 kN (86,844 lbf). Isp: 316 sec. Burn time: 430 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-105-5. Status: Out of production. Cost $ : 14.210 million. First Flight: 1967. Last Flight: 1983. No Launched: 49. No Failed: 1.
Used on Launch Vehicles:
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© Mark Wade, 1997 - 2007 except where otherwise noted.
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