Misplaced Pages

YF-209

Article snapshot taken from Wikipedia with creative commons attribution-sharealike license. Give it a read and then ask your questions in the chat. We can research this topic together.
Chinese liquid-fuel rocket engine
YF-209
Country of originChina
DesignerAcademy of Aerospace Liquid Propulsion Technology
StatusIn development
Liquid-fuel engine
PropellantLOX / CH4
CycleGas-generator cycle
Configuration
Chamber1
Performance
Thrust, vacuum825.3 kilonewtons (185,500 lbf)
Thrust, sea-level735 kilonewtons (165,000 lbf)
Specific impulse, vacuum329s
Specific impulse, sea-level293s
References
References

The YF-209 is a liquid cryogenic rocket engine burning liquid methane and liquid oxygen in a gas-generator cycle. The engine is designed for reusability and commercial use and is currently under development as of May 2024.

History

The YF-209 is designed for the commercial launch market in China with reusability in mind. It can be reused at least 30 times and can be restarted at least 3 times during the mission with deep throttle capabilities. The engine hot fire test was successfully completed in February 2023. Development has been prioritised in 2024 to meet the growing needs of the commercial launch market.

References

  1. "China's new rocket engines". www.b14643.de. Retrieved 22 May 2024.
  2. Curcio, Blaine (10 May 2023). "Commercial Launch at China Space Day: Rocketing Towards Launch Diversity". SpaceRef. Retrieved 22 May 2024.
  3. "中国航天发布三款商业液体火箭发动机_央广网". news.cnr.cn. Retrieved 22 May 2024.
  4. Jones, Andrew (27 April 2023). "Chinese state-owned academy makes rocket engines available to commercial space firms". SpaceNews. Retrieved 22 May 2024.
  5. "China completes largest thrust liquid engine's ignition test". www.ecns.cn. Retrieved 22 May 2024.
Rocket engines and solid motors for orbital launch vehicles
Liquid
fuel
Cryogenic
Hydrolox
(LH2 / LOX)
Methalox
(CH4 / LOX)
Semi-
cryogenic
Kerolox
(RP-1 / LOX)
Storable
Hypergolic (Aerozine,
UH 25, MMH, or UDMH
/ N2O4, MON, or HNO3)
Other
Solid
fuel
  • * Different versions of the engine use different propellant combinations
  • Engines in italics are under development
Categories: