Volume 43 Issue 4
Jul.  2023
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Article Navigation >  Chinese Journal of Space Science  > 2023  >  43(4): 711-723 Open Access
HUANG Jin, CHANG Liang, DONG Baiyang, LIU Zeyu, HAN Shengxing, SI Chaoming. Development on Space Environment and Its Dynamic and Thermal Problems of Ultra-LEO Satellites (in Chinese). Chinese Journal of Space Science, 2023, 43(4): 711-723 doi: 10.11728/cjss2023.04.2022-0010
Citation: HUANG Jin, CHANG Liang, DONG Baiyang, LIU Zeyu, HAN Shengxing, SI Chaoming. Development on Space Environment and Its Dynamic and Thermal Problems of Ultra-LEO Satellites (in Chinese). Chinese Journal of Space Science, 2023, 43(4): 711-723 doi: 10.11728/cjss2023.04.2022-0010
shu

Development on Space Environment and Its Dynamic and Thermal Problems of Ultra-LEO Satellites

doi: 10.11728/cjss2023.04.2022-0010 cstr: 32142.14.cjss2023.04.2022-0010

  • Innovation Academy for Microsatellites of Chinese Academy of Sciences, Shanghai 201203

  • Shanghai Engineering Center for Microsatellites, Shanghai 201203

  • Received Date: 2022-04-21
  • Rev Recd Date: 2022-06-30
    • Available Online: 2023-02-14
    Abstract
  • Ultra LEO spacecraft has become a hot research field for a wide range of application in military, remote sensing, scientific research, etc. Due to the special space environment of ultra-low orbit, many technical difficulties need to be solved, mainly focusing on atmospheric environment prediction, aerodynamic, aerothermal and so on. The main atmospheric models and inversion methods for typical ultra-low orbit vehicle missions are studied, and the model data is compared. By combining various cases of aerodynamic passive stability, the methods of aerodynamic calculation and the important impact of aerodynamic structural design are investigated. Aerodynamic design and stability control methods under aerodynamic interference are introduced. The aerodynamic thermal environment and simulation algorithms of ultra-low orbit satellites are studied, and various thermal resistant composite materials and their application scenarios are introduced. Detailed analyses were conducted on the technologies for variable switching of heat and heat dissipation for ultra-low orbit satellites, and the advantages and disadvantages of each scheme were briefly reviewed. This review is helpful to promote the key technology research and test demonstration of ultra LEO spacecraft, turning the ultra LEO spacecraft from test mission to space application mission as soon as possible.

     

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