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

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 13, 2026 at 23:21:27 UTC

Other

Sources

Title
FAA Annual Compendium of Commercial Space Transportation 2012
Url
https://www.faa.gov/about/office_org/headquarters_offices/ast/media/The_Annual_Compendium_of_Commercial_Space_Transporation_2012.pdf
Title
CNSA Long March Launch Vehicle Family
Url
https://www.cnsa.gov.cn/n6758968/n6758973/c6771770/content.html