General thermal design structure of satellite deck

• Main Authors: FU XIN, HAN SAISAI, CHEN ZHANSHENG, LAI JING, CHEN HAN, ZHOU BILEI, CAO JIANGUANG, XU WENJIE, ZHAI ZAITENG, GUI LIJIA
• Format: Patent
• Language: Chinese; English
• Published: 29.04.2022
• Subjects: AIRCRAFT; AVIATION; COSMONAUTICS; PERFORMING OPERATIONS; TRANSPORTING; VEHICLES OR EQUIPMENT THEREFOR

The invention provides a universal satellite deck thermal design structure, and relates to the field of satellite thermal control design. The universal satellite deck thermal design structure comprises a KS-ZA white paint layer, a multi-layer heat insulation assembly, a heat pipe network, a black paint layer, an aluminum honeycomb deck and a rotating mechanism. The heat pipe network is connected to the aluminum honeycomb cabin plate, a black paint layer is sprayed on the inner surface of the aluminum honeycomb cabin plate, a KS-ZA white paint layer is sprayed on the outer surface of the aluminum honeycomb cabin plate, and the multi-layer heat insulation assembly is connected to the outer surface of the aluminum honeycomb cabin plate through a rotating mechanism; the rotating mechanism drives the multiple layers of heat insulation assemblies to be unfolded and folded on the surface of the KS-ZA white paint layer, and therefore the size of the heat dissipation face of the aluminum honeycomb cabin plate is adjus