Payload LEO
45,000 kg
Payload GTO
13,600 kg
Assessment
Partially reusable orbital heavy-lift rocket (base configuration 7x2 with seven BE-4 engines). First flight on 16.01.2025, several orbital launches since.
Technical data
Height98 m
Diameter7 m
Liftoff thrust19,928 kN
Stages2
PropellantLOX/CH4 (stage 1), LOX/LH2 (stage 2)
ReusabilityPartially reusable
First flight2025
Lead time–
Provider launch sites
Cape Canaveral Space Force Station – Launch Complex 36 (LC-36)Launch Site One (Corn Ranch – West Texas)
Price
Price on requestPrices shown are the providers' official figures and are always non-binding – only the individual quote is binding.