Spacecraft Matrix Cable Assembly Process Research

Authors

  • Chenhua Zhang
  • Minghua Zhang
  • Zhanjun Xia
  • Huifang Du
  • Ran Zhang

DOI:

https://doi.org/10.54097/hset.v35i.7027

Keywords:

Spacecraft; Matrix Calbe; Assembly Process.

Abstract

The matrix calbe can effectively realize lightweight and high reliability of spacecraft cable network. This paper focus on the assembly process of matrix cable which has multi-line characteristics, introduce the assembly process and related parameters. The result was verified by appearance inspection, tensile test, voltage drop test and metallographic experiment. Make sure that the assemble process of the cable is high quality and reliability.

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References

Xu Fuxiang. Satellite Engineering[M]. Beijing: China Aerospace Press, 2002:48-49.

Wang Yingyan, Huang Yeping. Spacecraft Environmental Engineering,2013,30(2):200-202.

Q/W1457-2015 General technical requirements for spacecraft cable networks.

Zhang P, Chen X. Li F, Fu Z, Zhang W 2019 Configuration optimization design and verification of Chang'e 4 lander Baijiang Spacecraft Engineering (08) :3-4.

Fu C, Zhang L, Wu X 2019 Product assurance practice based on the mission characteristics of chang'e-4 Spacecraft Engineering (04) :1-3.

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Published

11-04-2023

Issue

Vol. 35 (2023): 6th International Conference on Computer Engineering, Information Science & Application Technology (ICCIA 2023)

Section

Articles

License

Creative Commons License

This work is licensed under a Creative Commons Attribution-NonCommercial 4.0 International License.