DBSE
Hardware/Vehicles/Chang Zheng 2F

Chang Zheng 2F

Retired

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

Total Launches
29
Success Rate
100%
Payload to LEO
9.2 t
First Flight
1999
Reusable
No

Interactive Model

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Specifications

Height51.2 m
Diameter3.35 m
Wet Mass464,000 kg
Payload to GTO3.5 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

Chang Zheng 2CVehicle familyChang Zheng 3Vehicle familyChang Zheng 2DVehicle familyChang Zheng 3AVehicle familyChang Zheng 3BVehicle familyChang Zheng 4BVehicle familyChang Zheng 4CVehicle familyChang Zheng 3CVehicle familyCASC / CALTManufacturerYF-25Engine

Data Sources for This Record

Specifications
GCAT / Wikipedia · verified quarterly
Launch History
LL2 API · updated every 6h
Engine Data
Manufacturer + Wikidata