Chang Zheng 3A
RetiredCASC / CALT · 3-stage orbital rocket · Part of the DF5 family
Total Launches
27
Success Rate
100%
Payload to LEO
—
First Flight
1994
Reusable
No
Specifications
Height52.5 m
Diameter3.35 m
Wet Mass240,000 kg
Payload to GTO2.3 t
Payload to SSON/A
ManufacturerCASC / CALT
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