Chang Zheng 12
ActiveCASC / SAST · 2-stage orbital rocket
Total Launches
10
Success Rate
100%
Payload to LEO
—
First Flight
2024
Reusable
No
Specifications
Height62 m
Diameter3.8 m
Wet Mass433,000 kg
Payload to GTO6 t
Payload to SSON/A
ManufacturerCASC / SAST
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