Payload LEO
27,200 kg
Payload SSO
22,300 kg
Payload GTO
15,300 kg
Assessment
ULA's current primary launch system; maiden flight 8 January 2024, several successful missions since. Modular design with 0 to 6 solid boosters (GEM-63XL). Designed for human-rating (crew, e.g.
Technical data
Height61.6 m
Diameter5.4 m
Liftoff mass546.7 t
Liftoff thrust4,893 kN
Stages2
PropellantLOX/methane (Centaur: LOX/LH2)
ReusabilityExpendable
First flight2024
Lead time–
Provider launch sites
Cape Canaveral SLC-41Vandenberg SLC-3E
Price
Price on requestPrices shown are the providers' official figures and are always non-binding – only the individual quote is binding.