Chang Zheng 6C
RetiredCASC / SAST · 2-stage orbital rocket · Part of the DF5 family
Total Launches
2
Success Rate
100%
Payload to LEO
1 t
First Flight
2024
Reusable
No
Specifications
Height29 m
Diameter3.35 m
Wet Mass103,000 kg
Payload to GTON/A
Payload to SSON/A
ManufacturerCASC / SAST
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
Data Sources for This Record
Specifications
GCAT / Wikipedia · verified quarterly
Launch History
LL2 API · updated every 6h
Engine Data
Manufacturer + Wikidata