Issue |
MATEC Web Conf.
Volume 316, 2020
2020 6th Asia Conference on Mechanical Engineering and Aerospace Engineering (MEAE 2020)
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Article Number | 04004 | |
Number of page(s) | 5 | |
Section | Aerospace Engineering | |
DOI | https://doi.org/10.1051/matecconf/202031604004 | |
Published online | 01 July 2020 |
Research on the Application of Carbon Foam Absorbing Materials in Wireless Testing of Spacecraft Thermal Vacuum Test
Beijing Institute of Space Environment Engineering, Beijing, 100094
a Corresponding author: to_cl2004@126.com
With the rise of mobile communication satellites and low-orbit Internet satellite constellations, wireless testing is required in spacecraft thermal vacuum test, and a comprehensive thermal testing environment for vacuum low-temperature absorption is needed. This paper clarifies the key parameters that need to be paid attention to in the application of vacuum absorbing materials under vacuum and low temperature environment, gives reference indexes, and puts forward the technical process and test results for the development of absorbing shroud.
Key words: carbon foam / thermal test / wireless test / absorbing shroud
© The Authors, published by EDP Sciences, 2020
This is an Open Access article distributed under the terms of the Creative Commons Attribution License 4.0, which permits unrestricted use, distribution, and reproduction in any medium, provided the original work is properly cited.
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