Movatterモバイル変換


[0]ホーム

URL:


Jump to content
WikipediaThe Free Encyclopedia
Search

YF-215

From Wikipedia, the free encyclopedia
Chinese liquid-fuel rocket engine
YF-215
Country of originChina
DesignerAcademy of Aerospace Liquid Propulsion Technology
AssociatedLVLong March 9
StatusIn development
Liquid-fuel engine
PropellantLOX /CH4
CycleFull-flowstaged combustion
Configuration
Chamber1
Performance
Thrust, sea-level2,000 kilonewtons (450,000 lbf)

TheYF-215 is aliquidcryogenicrocket engine burningliquid methane andliquid oxygen in afull-flow staged combustion cycle. The engine is currently under development and is designed to power thesuper-heavy launch vehicle Long March 9.

History

[edit]

The YF-215 engine has been designed to power the first stage of the Long March 9 rocket, with 26 of these engines in the first stage.[1] A successful ignition test of the pre-combustion chamber and gas generator of the engine was conducted on 12 May 2023.[2]

References

[edit]
  1. ^Jones, Andrew (27 November 2023)."China makes progress on Raptor-like engines for super heavy rocket".SpaceNews. Retrieved21 May 2024.
  2. ^Beil, Adrian (17 May 2023)."Beidou-3 G4 gets launched and Chinese Raptor gets tested, as it receives its own name".NASASpaceFlight.com. Retrieved21 May 2024.
Liquid
fuel
Cryogenic
Hydrolox
(LH2 /LOX)
Methalox
(CH4 /LOX)
Semi-
cryogenic
Kerolox
(RP-1 /LOX)
Storable
Hypergolic (Aerozine,
UH 25,MMH, orUDMH
/N2O4,MON, orHNO3)
Other
Solid
fuel
  • * Different versions of the engine use different propellant combinations
  • Engines initalics are under development
Retrieved from "https://en.wikipedia.org/w/index.php?title=YF-215&oldid=1225043053"
Categories:
Hidden categories:

[8]ページ先頭

©2009-2025 Movatter.jp