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Hardware/Vehicles/Chang Zheng 2C

Chang Zheng 2C

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CASC / CALT · 2-stage orbital rocket · Part of the DF5 family

Total Launches
89
Success Rate
97.8%
Payload to LEO
2.8 t
First Flight
1982
Reusable
No

Specifications

Height35.2 m
Diameter3.35 m
Wet Mass192,000 kg
Payload to GTON/A
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