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Hardware/Vehicles/Zhuque-3

Zhuque-3

Active

Landspace · 2-stage orbital rocket

Total Launches
2
Success Rate
100%
Payload to LEO
12 t
First Flight
2025
Reusable
Yes

Specifications

Height66.1 m
Diameter4.5 m
Wet Mass560,000 kg
Payload to GTON/A
Payload to SSON/A
ManufacturerLandspace
CountryChina

Engines Used

No engine records tracked for this vehicle yet.

    Engine usage data lives in the Engine Dashboard.

    Launch History

    Reliability by Year

    Related Entities

    LandspaceManufacturer

    Data Sources for This Record

    Specifications
    GCAT / Wikipedia · verified quarterly
    Launch History
    LL2 API · updated every 6h
    Engine Data
    Manufacturer + Wikidata