Chang Zheng 2D
ActiveCASC / SAST · 2-stage orbital rocket · Part of the DF5 family
Total Launches
105
Success Rate
99%
Payload to LEO
3.4 t
First Flight
1992
Reusable
No
Specifications
Height38.3 m
Diameter3.35 m
Wet Mass232,000 kg
Payload to GTON/A
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