Abstract
The thermal effect is one of the most concerning and studying the case of heat transfer and thermal deformation in the aerospace structure in general and the structure of artificial satellites in particular is fundamental for a space exploration mission. Heat can appear when satellites are affected by solar radiation and radiation from planets. For spatial structures, the theory of heat transfer has been applied quite effectively. In this study, we applied Finite Element Method for analyzing temperature distribution and thermal deformation by using commerce software. The results showed that the analysis on thermal effect of a selected satellite model with the temperature difference of two opposite sides on the structure of the satellite. Specifically, the temperature distribution and thermal deformation are presented for the three materials. Finally, we evaluate the effectiveness of materials applied to satellite structures.
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References
D.G. Gilmore, Spacecraft Thermal Control Handbook, vol. 1 (Fundamental Technologies, The Aerospace Corporation Press, California, 2002)
P. Grande, A. Sanz-Andrés, C. Guerra, G. Alonso, Analytical study of the thermal behaviour and stability of a small satellite. Appl. Thermal Eng. 29, 2567–2573 (2012)
L. Lijun, Y. Jun, Analysis and modeling of spacecraft with flexible solarpanel disturbed by thermally induced motion, in Proceedings of the 33rd Chinese Control Conference (Nan**g, China, 2014), pp. 6382–6387
G.F.Abdelal, et al., Thermal fatigue analysis of small-satellite structure. Int. J. Mech. Mater. Des. 3(2), 145–159 (2006)
G.F. Abdelal et al. Thermal fatigue analysis of solar panel structure for micro-satellite applications. Int. J. Mech. Mater. Des. 4(1), 53–62 (2008)
Acknowledgements
This research is funded by Hung Yen University of Technology and Education (UTEHY) under grant number UTEHY.L.2021.02. and Vietnam Academy of Science and Technology (Grant number VAST01.08/21–22)
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Van Bach Ngoc, P., Thien, N.L., Quan, P.H. (2024). Thermal Analysis on Small Satellite Structure Under Cosmic Radiation Effect. In: Long, B.T., et al. Proceedings of the 3rd Annual International Conference on Material, Machines and Methods for Sustainable Development (MMMS2022). MMMS 2022. Lecture Notes in Mechanical Engineering. Springer, Cham. https://doi.org/10.1007/978-3-031-39090-6_29
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DOI: https://doi.org/10.1007/978-3-031-39090-6_29
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