Chinese Space Science and Technology
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GUI Xiaohong 1 SONG Xiang′e2
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Abstract: Hightemperatureheatpipereceiversarecommonlyusedasacorecomponentofspacesolardynamicpowersystem.Onthebaseofheatconductiongoverningdifferentialequationundermicrogravity,two-dimensionalnumericalanalysisofPCMcontainerwasconductedbyaenthalpymethod.Withbothvoidcavityandphasechangeconsidered,thermalperformanceofheatpipereceiverwasanalyzed.NumericalresultswerecomparedwithNASAresults.Theaccuracyofcalculationmodelundergravitywasverified.Theresultsindicatethatvoidcavityinfluencestheprocessofphasechange.ThevoidcavityreducestheutilityandthermalstorageabilityofPCM.ThetemperaturegradientofPCMzoneisverysignificantbecauseofthevoidcavity.ThePCMcontainedintheintegratedheatpipeperformstheaveragingfunctionoftheheatloads.Normalworkingofwickensurestheuniformityofheatpipe,thusheatpipereceiveralleviatesthermalspotandthermalratcheting.
Key words: Spacesolarpowersystem, Heatpipereceiver, Phasechangematerial, Voidcavity, Phasechange, Spacecraft
GUI Xiao-Hong, SONG Xiang-E. TransientThermalAnalysisofHeatPipeReceiverunderMicrogravity[J]. Chinese Space Science and Technology, doi: 10.3780/j.issn.1000-758X.2015.04.007.
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URL: https://journal26.magtechjournal.com/kjkxjs/EN/10.3780/j.issn.1000-758X.2015.04.007
https://journal26.magtechjournal.com/kjkxjs/EN/Y2015/V35/I4/46