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 (2): 16-24.doi: 10.3969/j.issn.1671-0940.2022.02.003

• 专刊 • 上一篇    下一篇

Study on the Effect of Solid Particles on Jet Flow and Base Thermal Environment for Solid-Liquid Bundled Rocket 

  

  • 出版日期:2022-10-13 发布日期:2022-10-14

Study on the Effect of Solid Particles on Jet Flow and Base Thermal Environment for Solid-Liquid Bundled Rocket 

  1. 1 Aerospace System Engineering Shanghai, Shanghai 201108

    2 Shanghai Academy of Spaceflight echnology, Shanghai 201108

    3 Nanjing University of Science and Technology, Nanjing 210094 

  • Online:2022-10-13 Published:2022-10-14
  • About author:ZHANG Liang (1977− ), received his Doctor’s degree from Shanghai Jiaotong University. He is mainly engaged in the research of launch vehicle system design.

Abstract: Compared with using liquid rocket engines, there are a lot of high-temperature solid particles in the solid-liquid bundled rocket, which make the rocket base thermal environment worse. In order to study the influence of high-temperature solid particles on the base thermal environment, firstly, the effect of particle diameter on the jet distribution and the thermal environment in a single solid motor jet was analyzed using a numerical simulation method, and the results were compared with those of a ground test. Further, the effects of high-temperature solid particles on the jet and the thermal environment of the solid-liquid bundled rocket were analyzed and compared with flight data. The results show that high-temperature solid particles can increase the jet temperature and reduce the jet velocity. The larger the particle diameter, the greater the impact on the jet core temperature. The role of high-temperature solid particles cannot be ignored in the study of the base thermal environment.

Key words: font-family:arial, helvetica, sans-serif, font-size:15px, background-color:#FAFAFA, ">solid rocket motor, thermal environment, two-phase flow, solid-liquid bundled rocket