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Long March 3 original configuration

The original Long March 3 combined Long March 2C-derived lower stages with China's first cryogenic liquid-hydrogen and liquid-oxygen upper stage. It introduced restartable cryogenic propulsion and China's capability to place spacecraft into geosynchronous transfer orbit before being retired in favor of the 3A series.

Identity

Aliases
Original Long March 3Chang Zheng 3CZ-3LM-3长征三号
Family Name
Long March 3
Full Name
Long March 3 original configuration
Reusability
expendable
Slug
long-march-3-original
Status
retired
Type
rocket
Variant Name
Original

Details

Description
The original Long March 3 combined Long March 2C-derived lower stages with China's first cryogenic liquid-hydrogen and liquid-oxygen upper stage. It introduced restartable cryogenic propulsion and China's capability to place spacecraft into geosynchronous transfer orbit before being retired in favor of the 3A series.
Diameter M
3.35
First Flight Year
1,984
Height M
44.86
Last Flight Year
2,000
Liftoff Mass Kg
204,880
Manufacturer Id
jd7fbrt32syts4rtsgsh4m023n7kqwpa
Parent Vehicle Family Id
nd7xvvkd68vwhvfye5863w7p5h8aey9m
Payload Capacity Kg
Gto
1,600
Stages Count
3
Strap On Boosters Count
0

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Creation Time
7/14/2026, 6:26:56 AM
Updated Time
7/14/2026, 6:26:56 AM