Abstract
Using a thermal-vacuum test and Monte Carlo simulation analysis, this paper examined the key technical performance parameters of the carbon-fiber heating cage and compared them with those of the traditional nickel-chromium alloy heating cage. The results indicated that the heating capacity and temperature uniformity of the carbon-fiber heating cage for spacecraft were better than those of the traditional nickel-chromium alloy heating cage, and that the electro-thermal properties of the carbon-fiber infrared heating cage met the requirements of the spacecraft thermal-vacuum environment.
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Xu, F., Xia, Y., Liu, G., Li, Y., Chen, J., Liu, C. (2020). Study of Key Technological Performance Parameters of Carbon-Fiber Infrared Heating Cage. In: Liang, Q., Wang, W., Liu, X., Na, Z., Jia, M., Zhang, B. (eds) Communications, Signal Processing, and Systems. CSPS 2019. Lecture Notes in Electrical Engineering, vol 571. Springer, Singapore. https://doi.org/10.1007/978-981-13-9409-6_19
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DOI: https://doi.org/10.1007/978-981-13-9409-6_19
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