Long March 2E Second Stage
The Long March 2E second stage is the upper liquid-propellant stage of the retired two-stage LM-2E launcher. CNSA establishes the two-stage N2O4/UDMH architecture; this record intentionally avoids attributing an engine model not asserted by the source.
Identity
- Domains
- spaceflight
- Identity Level
- integrated-system
- Kind
- integrated-propulsion-system
- Name
- Long March 2E Second Stage
- Status
- retired
Details
- Description
- The Long March 2E second stage is the upper liquid-propellant stage of the retired two-stage LM-2E launcher. CNSA establishes the two-stage N2O4/UDMH architecture; this record intentionally avoids attributing an engine model not asserted by the source.
- Propellants
- N2O4UDMH
Assets & Meta
- Creation Time
- August 13, 2026 at 23:28:21 UTC
- Updated Time
- August 13, 2026 at 23:28:21 UTC
Other
- Sources
- Title
- CNSA Long March-2E
- Title
- CNSA Long March-2E (Chinese technical page)