Zhuque-2E

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Payload LEO

6,000 kg

Payload SSO

4,000 kg

Assessment

Methane/liquid-oxygen medium-class rocket; in service since 2024 and successor to the retired baseline Zhuque-2. LEO figure at 200 km, SSO figure at 500 km.

Source (provider information)

Technical data

Height47.8 m

Diameter3.4 m

Liftoff mass220 t

Liftoff thrust2,880 kN

Stages2

PropellantMethalox (LOX/CH4)

ReusabilityExpendable

First flight2024

Lead time–

Provider launch sites

Jiuquan Satellite Launch Center – Launch Complex 96AJiuquan Satellite Launch Center – Launch Complex 96B

Price

Price on request

To the provider: LandSpace

Prices shown are the providers' official figures and are always non-binding – only the individual quote is binding.