AEROSPACE CHINA

中国航天科技集团有限公司主管

中国航天系统科学与工程研究院主办

ISSN 1671-0940

CN 11-4673/V

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AEROSPACE CHINA ›› 2022, Vol. 23 ›› Issue (1): 19-26.doi: 10.3969/j.issn.1671-0940.2022.01.003

• 中国载人航天 • 上一篇    下一篇

Development of Solid Rocket Motor for Manned Launch Vehicle Escape System

  

  • 出版日期:2022-07-20 发布日期:2022-07-20

Development of Solid Rocket Motor for Manned Launch Vehicle Escape System

  1. Xi’an Aerospace Solid Propulsion Technology Institute, Xi’an 710025
  • Online:2022-07-20 Published:2022-07-20
  • About author:LI Dongchun (1982− ), senior engineer, graduated from Academy of Aerospace Solid Propulsion Technology with a Master degree. He is mainly engaged in the research on solid rocket motors.

Abstract: The solid rocket motors for the escape system of China’s LM-2F manned launch vehicle are described, the key technologies and technical innovations utilized are summarized. The technical features and development of foreign manned launch abort systems are also presented. The development trends of the solid rocket motor for future Chinese manned launch vehicle escape systems are proposed, which can provide a reference for the future development of manned launch vehicle escape systems.

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