Atlas CCB

home
topic index

Model: Atlas CCB. 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. Motor: RD-180. Status: Active. First Flight: 2002. Last Flight: 2007. No Launched: 17.

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:

Atlas V.

Contact us with any corrections, additions, or comments.

Conditions for use of drawings, pictures, or other materials from this site..
To contact astronauts or cosmonauts.

© Mark Wade, 1997 - 2008 except where otherwise noted.