FIELD: space technology.
SUBSTANCE: invention relates to space technology, and more specifically to the thermal control systems of spacecraft. The power thermal panel of the spacecraft contains a skin with a radiation-emitting surface and heat pipes. The thermal panel is made in the form of a monolithic structure that combines the skin with heat pipes into a single whole. The heat pipes are made in the form of a lattice system of mutually intersecting heat pipes connected by a common internal cavity and forming a closed evaporation-condensation system filled with a coolant. The thermal panel on the upper surface of the skin has space for the installation of equipment.
EFFECT: increased efficiency of the thermal conduction model is achieved.
4 cl, 2 dwg
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