The calculations of radiator surface area and heat insulation layer thickness are necessary for the design of passive thermal control system.
纳卫星的被动热控系统对卫星舱内的温度控制及其有效载荷的可靠工作具有重要意义。
In this paper the rationale of thermal insulation using aluminium foil as well as the calculation of RK values is described, and the rational thickness values of the air interface layer are presented.
本文讨论了用铝箔隔热的基本原理和R _ k值的计算，提出了表面贴铝箔的绝热空气间层的合理厚度值。
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