This page no longer updated from 31 October 2001. Latest version can be found at www.astronautix.com
Gross Mass: 306,914 kg.
Empty Mass: 22,461 kg. Thrust (vac): 423,386 kgf. Isp: 338 sec. Burn time: 253 sec. Propellants: Lox/Kerosene Isp(sl): 311 sec. Diameter: 3.8 m. Span: 3.8 m. Length: 32.5 m. Country: USA. No Engines: 1. RD-180 Status: Development. Comments: 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.
Back to Index
Last update 12 March 2001.
Contact Mark Wade with any corrections or comments.
Conditions for use of drawings, pictures, or other materials from this site..
© Mark Wade, 2001 .