YF-24E
The YF-24E is the liquid-propellant second-stage engine identified for the Long March 2C launch vehicle. It burns nitrogen tetroxide and unsymmetrical dimethylhydrazine; this record preserves the supported vehicle-specific model without inferring unreported cycle or performance details.
Identity
- Aliases
- YF-24EYF24EYF-24E liquid rocket engine
- Domains
- spaceflight
- Identity Level
- model
- Kind
- liquid-rocket-engine
- Name
- YF-24E
- Status
- active
Details
- Description
- The YF-24E is the liquid-propellant second-stage engine identified for the Long March 2C launch vehicle. It burns nitrogen tetroxide and unsymmetrical dimethylhydrazine; this record preserves the supported vehicle-specific model without inferring unreported cycle or performance details.
- Propellants
- N2O4UDMH
Assets & Meta
- Creation Time
- August 13, 2026 at 23:21:27 UTC
- Updated Time
- August 22, 2026 at 08:42:53 UTC
Other
- Sources
- Title
- FAA Annual Compendium of Commercial Space Transportation 2012
- Title
- CNSA Long March Launch Vehicle Family