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Bin Li

Academy of Aerospace Propulsion Technology, China

 

Brief Biography:
Bin Li, research fellow and doctoral supervisor, member of the "National Ten Thousand Talents Program" (for Science and Technology Innovation Leaders), is currently the Director of the Science and Technology Commission of The China Academy of Aerospace Propulsion Technology. He has been engaged in the technical research of advanced liquid rocket engines for a long time, and led the team successfully developed the 120-ton high-pressure staged-combustion LOX-kerosene engine, which are employed as the main propulsion system for the new generation Long March launch vehicles. At present, Bin Li is committed to tackling key technologies for propulsion system of manned lunar missions and heavy launch vehicles. He has won a first prize of National Science and Technology Progress Award and 15 National Defense Science and Technology Progress Awards, published more than 50 papers and 3 monographs, and was granted with 35 invention patents. He was honored the 4th Aerospace Laureate Awards, the Qian Xuesen Outstanding Contribution Award from China Aerospace Foundation, and other awards.

 

Speech Title:
Key Technologies of Advanced Liquid Rocket Engines

 

Abstract:
The liquid rocket engine is the core component of launch vehicles and determines the ability to enter space. With the rapid development of large-scale space infrastructure and the aerospace industry, higher requirements are imposed on liquid propulsion technology. This lecture provides a systematic overview of the major research directions of advanced liquid rocket engines. Beginning with an overview of Chinese liquid rocket engines, the speech addresses representative technical characteristics of advanced liquid rocket engines, including rapid dynamic processes, extreme operating environments, high requirements on manufacturing, and difficulties in fault diagnosis. To overcome these challenges, several research directions have been identified. The speech introduces the latest progress in detail and outlines prospects for future advancement, covering the control of system dynamic characteristics, the design of lightweight structures, the control of combustion stability, the design of high-power-density turbopumps, technologies of reusable engines, as well as fault diagnosis and health management.

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