| Citation: | HAN X，ZHOU Y，HUANG H，et al. Design and verification of high-precision dynamic temperature control system[J]. Journal of Beijing University of Aeronautics and Astronautics，2025，51（5）：1539-1547 （in Chinese） doi: 10.13700/j.bh.1001-5965.2023.0297
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A high-precision dynamic temperature control system is proposed, developed, and tested with the goal of addressing the issue that the existing ground temperature environment simulation equipment finds it challenging to realize the temperature deviation test of scientific loads with extremely high temperature control accuracy in deep space exploration. The system uses a liquid nitrogen cold plate as the cold source, and it realizes the high precision static and dynamic temperature control on the 300mm×300mm contact surface by means of electric heating, heat pipe heat transfer, and solid structure heat conduction. The test results demonstrate that the temperature control system can accomplish high-precision temperature stability control with a temperature variation of less than ±0.001℃ within the contact surface temperature range of −10～45 °C. In addition, it can also realize the linear control of temperature rise and fall rate of ± 0.05 ℃/1 000 s～1 ℃/1 000 s on the load contact surface. Compared with the set temperature curve, the whole-process temperature tracking error is less than 0.003 ℃ and 0.04 ℃. The established temperature control system has the ability to conduct high-precision temperature dynamic deviation tests. It will have good application prospects in tasks such as deep space exploration payload development and testing.
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