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Atlas CCB
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Gross Mass: 306,914 kg (676,629 lb). Empty Mass: 22,461 kg (49,518 lb). Thrust (vac): 4,151.998 kN (933,406 lbf). Isp: 338 sec. Burn time: 253 sec. Propellants: Lox/Kerosene. Isp(sl): 311 sec. Diameter: 3.81 m (12.49 ft). Span: 3.81 m (12.49 ft). Length: 32.46 m (106.49 ft). Country: USA. No Engines: 1. Engine: RD-180. Status: In production. First Flight: 2002. Last Flight: 2006. No Launched: 8. Common Core Booster uses Glushko RD-180 engine and new isogrid tanks. Used in Atlas IV/USAF EELV, Atlas V. Includes 272 kg booster interstage adapter and 1297 kg Centaur interstage adapter.
Used on Launch Vehicles:
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© Mark Wade, 1997 - 2007 except where otherwise noted.
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