Atlas CCB

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Atlas CCB

LOx/Kerosene propellant rocket stage. 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.

Status: Active. Thrust: 4,152.00 kN (933,406 lbf). Gross mass: 306,914 kg (676,629 lb). Unfuelled mass: 22,461 kg (49,518 lb). Specific impulse: 338 s. Specific impulse sea level: 311 s. Burn time: 253 s. Height: 32.46 m (106.49 ft). Diameter: 3.81 m (12.49 ft). Span: 3.81 m (12.49 ft).

Country: USA. Engines: RD-180. Launch Vehicles: Atlas V 401, Atlas V 521, Atlas V 431, Atlas V 411, Atlas V 501. Propellants: Lox/Kerosene.

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