Chinese Space Science and Technology ›› 2015, Vol. 35 ›› Issue (6): 12-.doi: 10.3780/j.issn.1000-758X.2015.06.002
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ZHANG Hong-Sheng, LI Yun-Ze, WANG Sheng-Nan, NING Xian-Wen
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Abstract: Toimprovethetemperaturecontrolreliabilityofspacecraftthermalcontrolsystem,aselfadaptiontemperaturecontrolcoldplatewasdesignedbasedonthevolumechangecharacteristicsoftheparaffinwaxduetothephasechangeasitstemperaturechanged.Thedesignmodeloftheselfadaptiontemperaturecontrolcoldplatewasbuilt,andthethermalnetmodelofthesinglephasefluidloopwiththecoolplatewasgiven.Theperformanceofthecoldplateandthesinglephasefluidloopwasanalyzed.Resultsshowthatthecoldplatedesignedhastheabilityofselfadaptiontemperaturecontrol,anditmaybewidelyusedinthetemperaturecontrolfortheelectronicdevicesatgroundandheatloadsonspacecraft.
Key words: Selfadaptiontemperaturecontrol, Thermalcontrol, Sensitiveparaffinwax, Coldplate;Spacecraft
ZHANG Hong-Sheng, LI Yun-Ze, WANG Sheng-Nan, NING Xian-Wen. DesignandPerformanceAnalysisofSelfadaptionTemperatureControlColdPlate[J]. Chinese Space Science and Technology, 2015, 35(6): 12-.
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URL: https://journal26.magtechjournal.com/kjkxjs/EN/10.3780/j.issn.1000-758X.2015.06.002
https://journal26.magtechjournal.com/kjkxjs/EN/Y2015/V35/I6/12