Thermal design and analysis of JZJ-5 CubeSat

Abstract JZJ-5 is a 3U commercial CubeSat contracted by Nanjing University of Science and Technology. This paper first introduces the thermal control design of the CubeSat, then calculates the temperature field in the high and low temperature conditions by using the finite element method, and finally compares the measured temperature data in orbit with the thermal simulation data. The data results show that the temperature state of the CubeSat in orbit meets the requirements of thermal design, and the thermal control design scheme and simulation model are reasonable.