The invention relates to a satellite thermal control system and a satellite. The satellite thermal control system comprises a magnetic bar thermal control module and a magnetic bar arranged on a satellite, and the magnetic bar thermal control module is used for adjusting the temperature of the magnetic bar; the propulsion thermal control module is arranged in a propulsion system of the satellite, and the propulsion thermal control module is used for adjusting the temperature of the propulsion system; the battery thermal control module is arranged on a battery of the satellite, and the battery thermal control module is used for adjusting the temperature of the battery; the battery controller thermal control module is arranged on a battery controller of the satellite, and the battery controller thermal control module is used for adjusting the temperature of the battery controller; and the antenna thermal control module is arranged on an antenna of the satellite, and the antenna thermal control module is used for adjusting the temperature of the antenna. According to the satellite thermal control system, the temperature of the equipment on the satellite can be adjusted, so that the equipment on the satellite can be exposed in an external space environment, and normal operation of the satellite is guaranteed.
本申请涉及一种卫星热控系统及卫星。卫星热控系统包括:磁棒热控模块,设置于卫星的磁棒,磁棒热控模块用于调整磁棒的温度;推进热控模块,设置于卫星的推进系统,推进热控模块用于调整推进系统的温度;电池热控模块,设置于卫星的电池,电池热控模块用于调整电池的温度;电池控制器热控模块,设置于卫星的电池控制器,电池控制器热控模块用于调整电池控制器的温度;天线热控模块,设置于卫星的天线,天线热控模块用于调整天线的温度。本申请的卫星热控系统能够对卫星上的设备进行温度调整,以使卫星上的设备可以暴露在外空间环境中,保证卫星正常运行。
Satellite thermal control system and satellite
一种卫星热控系统及卫星
2024-01-12
Patent
Electronic Resource
Chinese
IPC: | B64G Raumfahrt , COSMONAUTICS |
Satellite thermal control handbook
SLUB | 1994
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TIBKAT | 1994
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