One of the key problems in the design of nanosatellites is to provide a specified temperature range for the operation of electronic equipment. In structures of modern nanosatellites mainly used the elemental base of smartphones. To process a large amount of information, more advanced processors with high thermal power are required. The specified thermal mode of the on-board computer can be achieved using a remote heat removal system or by direct contact of the processor cover with the carbon fiber reinforced plastics (CFRP) body of the nanosatellite. Using a model of nanosatellite as an example, a thermal control system with miniature loop heat pipes and highly heat-conducting refrigerators-emitters is designed. The influence of the thermal conductivity coefficient in the reinforcement plane of the nanosatellite CFRP body on its temperature state in low Earth orbit is studied.
CITATION STYLE
Yu, W., Soe-Moe, Z., Denisov, O. V., & Denisova, L. V. (2020). Research of thermal control system for nanosatellite with carbon fiber reinforced plastic body. In IOP Conference Series: Materials Science and Engineering (Vol. 934). IOP Publishing Ltd. https://doi.org/10.1088/1757-899X/934/1/012056
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