ChangZheng 2C
ChangZheng 2C
Space Launch Systems
Basic Information
Name
ChangZheng 2C
Designation
ChangZheng 2C
Alternate Designation
CZ-2C, Long March 2C
Equipment Type
Space Launch Systems
Manufacturer
CALT
Date of Introduction
1983
Description
The ChangZheng 2C, also known as the CZ-2C or Long March 2C (LM-2C) in the West, is a space launch vehicle capable of carrying payloads of 3+ tons to Low Earth Orbits (LEO). The first launch of the 1-core CZ-2C rocket was carried out in 1982.
Overview (Deagel)
Group
Space Launch Systems
Status
Active
Also Known As
CZ-2C, Long March 2C
Origin
China
Contractor
CALT
Initial Operational Capability (IOC)
1983
First Flight
1982
Total Production
76
Specifications (Deagel)
Number of Stages
2
Dimensions — Height
42 meter
Dimensions — Rocket Diameter
3.4 meter
Mass — Max Lift-off Weight
233 ton
Mass — Payload to GTO
1,250 kilogram
Mass — Payload to LEO
3,800 kilogram
Mass — Payload to SSO
1,900 kilogram
Variants
Variant 1
ChangZheng 2C
Variant 2
ChangZheng 2D
Variant 3
ChangZheng 2F
Details
Country of Origin
China
Sources
deagel.com: https://www.deagel.com/x/x/a002554
Classification
Domain
Air & Air Defense
Equipment Status
Active
Dimensions
Length
—
Width
3.4 m
Height
42 m
Weight
233000 kg
Operators (1)
China
Something went wrong. Please reload the page.
Reload