ChangZheng 4C
ChangZheng 4C
Space Launch Systems
Basic Information
Name
ChangZheng 4C
Designation
ChangZheng 4C
Alternate Designation
CZ-4C, Long March 4C
Equipment Type
Space Launch Systems
Manufacturer
SAST
Date of Introduction
2006
Description
The ChangZheng 4C, also known as the CZ-4C or Long March 4C (LM-4C) in the West, is a further evolution of the ChangZheng 4B rocket. The first launch of the improved rocket was carried out in 2006.
Overview (Deagel)
Group
Space Launch Systems
Status
Active
Also Known As
CZ-4C, Long March 4C
Origin
China
Contractor
SAST
Initial Operational Capability (IOC)
2006
First Flight
April 26, 2006
Total Production
53
Specifications (Deagel)
Number of Stages
3
Dimensions — Height
45.8 meter
Dimensions — Rocket Diameter
3.4 meter
Mass — Max Lift-off Thrust
2,961 kN
Mass — Max Lift-off Weight
250 ton
Mass — Payload to GTO
1,500 kilogram
Mass — Payload to LEO
4,200 kilogram
Mass — Payload to SSO
2,800 kilogram
Variants
Variant 1
ChangZheng 4B
Variant 2
ChangZheng 4C
Details
Country of Origin
China
Sources
deagel.com: https://www.deagel.com/x/x/a002556
Classification
Domain
Air & Air Defense
Equipment Status
Active
Dimensions
Length
45.8 m
Width
3.4 m
Height
45.8 m
Weight
250000 kg
Operators (1)
China
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