Payload LEO
7,000 kg
Payload SSO
3,000 kg
Assessment
Medium-lift liquid-propellant rocket (RP-1/LOX, seven Welkin engines) with a partially reusable first stage (landing legs/grid fins); first flight planned for 2026.
Technical data
Height42 m
Diameter3.4 m
Liftoff mass283 t
Liftoff thrust3,434 kN
Stages2
PropellantLOX/RP-1
ReusabilityPartially reusable
Lead time–
Provider launch sites
Dongfeng Commercial Space Innovation Test Area (Jiuquan)Jiuquan Satellite Launch CenterOriental Spaceport Haiyang (sea launch – Yellow Sea)
Price
Price on requestPrices shown are the providers' official figures and are always non-binding – only the individual quote is binding.