Misplaced Pages

YF-130

Article snapshot taken from[REDACTED] 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 rocket engine
YF-130
Country of originChina
ManufacturerAcademy of Aerospace Liquid Propulsion Technology
ApplicationLong March 9
StatusUnder development
Liquid-fuel engine
PropellantLiquid oxygen / Kerosene
Mixture ratio2.62
CycleStaged combustion
Pumps1
Configuration
Chamber2
Performance
Thrust, sea-level~5,000 kilonewtons (1,100,000 lbf)
Thrust-to-weight ratio78
Chamber pressure22 MPa (3,200 psi)
Specific impulse308
Dimensions
Length~4.3 m (14 ft)
Diameter~3–3.3 m (9.8–10.8 ft)
Dry mass~6.5 t (6.4 long tons; 7.2 short tons)
Used in
Long March 9 First stage and booster
References
Notes

The YF-130 is a Chinese rocket engine fueled by LOX and kerosene in an oxidizer-rich staged combustion cycle currently in development. It has been designed to reach around 500 tonnes of thrust and it will power the super heavy Long March 9 rocket.

History

Chinese researchers completed a "half-system on full working condition" test of a YF-130 engine in March 2021, and expected to finish a whole-system test verification by the end of the year. Full system test has been successfully completed on November 6, 2022.

References

  1. 李斌,陈晖,马冬英,高玉闪 (2022-01-03). "500tf级液氧煤油高压补燃发动机研制进展" (in Simplified Chinese). 《火箭推进》2022年02期. Retrieved 2022-06-09.{{cite web}}: CS1 maint: multiple names: authors list (link)
  2. "以重型之力,夯强国之基|深度解码我国最大推力液体火箭发动机" (in Simplified Chinese). 西安航天动力研究所. 2022-11-06. Retrieved 2022-11-06.
  3. "China moves to next stage of super heavy rocket development". SpaceNews. 14 January 2021.
  4. Zhen, Liu (23 December 2021). "China closes in on deep space ambitions with latest rocket engine test". South China Morning Post. Retrieved 13 March 2022.
  5. Xin, Ling (6 November 2022). "Powerful Chinese space rocket engine passes 'milestone' test". South China Morning Post. Retrieved 23 November 2022.
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
Stub icon

This rocketry article is a stub. You can help Misplaced Pages by expanding it.

Categories:
YF-130 Add topic