| Citation: | SHEN Chunmei, YU Feng, LIU Wenkaiet al. Thermal control system design and on-orbit verification of hyperspectral greenhouse gas monitor on FY-3D satellite[J]. Journal of Beijing University of Aeronautics and Astronautics, 2020, 46(11): 2026-2038. doi: 10.13700/j.bh.1001-5965.2020.0138(in Chinese)
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The structure layout of hyperspectral greenhouse gas monitor on FY-3D satellite is very compact. There are eight optical lens, twelve electronic devices and three motors in the small-scale space. There are so many optical lens with high-precision temperature control requirement and so many heat source equipment. And thermal control resources such as heating power and radiator layout space are limited. These above characteristics make thermal control system design of hyperspectral greenhouse gas monitor a challenge. Thermal control system was designed based on multiple design methods including thermal management, indirect radiation thermal control, radiation cooling and collaborative optimization design of integrated structural and thermal control. Thermal control difficult problems were solved effectively. Hyperspectral greenhouse gas monitor experienced multiple operating modes after entering orbit. On-orbit temperature data show that all components' temperatures meet the requirements, and optical lens have high temperature stability under all the experienced operating modes. The maximum temperature fluctuation of interferometer is within ±0.15℃ under normal operating mode, and it is within ±0.45℃ for other optical lens. Furthermore, no matter under standby mode in a whole orbit period or normal operating mode, the heat dissipation systems of two sets of electronic device designed based on thermal management do not need to consume thermal control power resources. High-precision thermal control and energy saving thermal design are realized under the condition of multiple heat sources and complex working mechanism.
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