›› 2015, Vol. 35 ›› Issue (6): 12-.doi: 10.3780/j.issn.1000-758X.2015.06.002
Previous Articles Next Articles
ZHANG Hong-Sheng, LI Yun-Ze, WANG Sheng-Nan, NING Xian-Wen
Received:
Revised:
Published:
Online:
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]. , 2015, 35(6): 12-.
0 / / Recommend
Add to citation manager EndNote|Reference Manager|ProCite|BibTeX|RefWorks
URL: http://journal26.magtechjournal.com/kjkxjs/EN/10.3780/j.issn.1000-758X.2015.06.002
http://journal26.magtechjournal.com/kjkxjs/EN/Y2015/V35/I6/12