Common Booster Core

Common Booster Core
Producent

Boeing, United Launch Alliance

Człon rakiet

Delta IV

Materiały napędowe

LH2, LOX

Rok pierwszego startu

2002

Osiągi
Siła ciągu przy starcie

3312,76 kN

Impuls właściwy w próżni

367 s

Wymiary
Długość

40,8 m

Średnica

5,1 m

Masa maksymalna

226400 kg

Silniki
Silnik 1.

RS-68

Stopień CBC Delty IV

Common Booster Core (CBC) – modułowy główny stopień rakiet nośnych Delta IV i dopalacz rakiet Delta IV Heavy. Wprowadzony do użytku w 2002. Wykorzystuje silnik RS-68 zasilany wodorem i tlenem.

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