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Long March 3 Stage 3

The retired Long March 3 third stage is the cryogenic upper propulsion stage of the three-stage LM-3 launcher. CNSA states that it uses liquid hydrogen and liquid oxygen and supports multiple ignitions; this integrated record does not infer a specific engine model.

Identity

Domains
spaceflight
Identity Level
integrated-system
Kind
integrated-propulsion-system
Name
Long March 3 Stage 3
Status
retired

Details

Description
The retired Long March 3 third stage is the cryogenic upper propulsion stage of the three-stage LM-3 launcher. CNSA states that it uses liquid hydrogen and liquid oxygen and supports multiple ignitions; this integrated record does not infer a specific engine model.
Propellants
LH2LOX

Assets & Meta

Creation Time
August 13, 2026 at 23:43:43 UTC
Updated Time
August 13, 2026 at 23:43:43 UTC

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