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Long March 12

The original Long March 12 is a two-stage liquid-oxygen and kerosene launch vehicle developed by the Shanghai Academy of Spaceflight Technology within CASC. It introduced China's first roughly four-meter-class launch-vehicle body and serves large low-orbit and sun-synchronous payloads from Hainan's commercial launch site.

Long March 12
Xiaojun Wang / China Academy of Launch Vehicle Technology · Creative Commons Attribution 4.0 International; the exact Wikimedia Commons record identifies this byte-matched image as “Long March 5 rolling out at Wenchang Space Launch Site,” authored by Xiaojun Wang of the China Academy of Launch Vehicle Technology, and records the CC BY 4.0 licence. Sharing and adaptation are permitted with appropriate attribution, a licence link, and an indication of changes; do not imply endorsement. The Commons record’s source note identifies the image as cropped from the cited DOI source. · Source
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Identity

Aliases
Chang Zheng 12CZ-12LM-12长征十二号
Family Name
Long March 12
Full Name
Long March 12
Status
active
Type
rocket
Variant Name
Base

Details

Description
The original Long March 12 is a two-stage liquid-oxygen and kerosene launch vehicle developed by the Shanghai Academy of Spaceflight Technology within CASC. It introduced China's first roughly four-meter-class launch-vehicle body and serves large low-orbit and sun-synchronous payloads from Hainan's commercial launch site.
Dimensions
Diameter
…
Height
…
First Flight Year
2,024
Manufacturer
Parent Vehicle Family
Propulsion Configurations
  • Entries
    • Count
      1
      Placement
      other
      Propulsion System
      Role
      main
      Stage
      all-stages
      Variant Notes
      System-level count 1; source states four first-stage engines but does not identify every stage model.
    Name
    Long March 12 standard two-stage integrated configuration
    Notes
    CASC describes a two-stage LOX/kerosene launcher with four 1,250 kN pump-after-swing first-stage engines. The integrated entry keeps the family relationship exact without inferring an unnamed second-stage engine model.
Rocket Specs
Payload Capacity
LEO
…
SSO
…
Reusability
expendable
Stages Count
2

Links

Assets & Meta

Creation Time
July 13, 2026 at 11:47:47 UTC
Updated Time
August 14, 2026 at 00:15:09 UTC