Zhuque-2
RetiredLandspace · 2-stage orbital rocket · Part of the ZQ-2 family
Total Launches
3
Success Rate
66.7%
Payload to LEO
—
First Flight
2022
Reusable
No
Interactive Model
Specifications
Height49.5 m
Diameter3.35 m
Wet Mass216,000 kg
Payload to GTON/A
Payload to SSON/A
ManufacturerLandspace
CountryChina
Engines Used
Engine usage data lives in the Engine Dashboard.
Launch History
Reliability by Year
Related Entities
Data Sources for This Record
Specifications
GCAT / Wikipedia · verified quarterly
Launch History
LL2 API · updated every 6h
Engine Data
Manufacturer + Wikidata