Small satellite load thermal control system

• Main Authors: YU MENGXIAO, QI JIANHUA, LIU JIE, TIAN MINLI, ZHANG CHAO
• Format: Patent
• Language: Chinese; English
• Published: 27.05.2022
• Subjects: AIRCRAFT; AVIATION; COSMONAUTICS; PERFORMING OPERATIONS; TRANSPORTING; VEHICLES OR EQUIPMENT THEREFOR

The invention provides a moonlet load thermal control system. The moonlet load thermal control system comprises a structural plate, a phase change module and a uniform temperature film, the structural plate is made of a heat conduction material, the structural plate is provided with a containing space, the containing space is provided with an opening, the phase change module is arranged in the containing space, and the temperature equalizing film is arranged on one side of the structural plate and arranged around the opening; the first functional device can abut against the side, away from the structural plate, of the uniform temperature film, and the second functional device can abut against the side, away from the bottom wall of the containing space, of the phase change module. Heat generated by the first functional device can be quickly transmitted to the structural plate through the temperature equalizing film, heat generated by the second functional device can be quickly transmitted to the structural pla