This subsystem studies the thermic variations that the nanosat will experience in orbit, related to the heat sources that exist in space.

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This subsystem must ensure that every component of the nanosat stays in the operational ranges throughout the mission, even while our system is subject to extreme thermal conditions.

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For this, Thermal’s team carry out simulations and calculations, in which the conduction, convection and radiation phenomenons are analyzed, to design a thermal control using elements such as paints, heathers, insulators, etc.