{"title":"Thermal Design and Thermal Analysis of Space Observation Equipment","authors":"徐. X. Zhen","doi":"10.3788/OMEI20112811.0063","DOIUrl":null,"url":null,"abstract":"On the research of observation equipment,the method of heat conduction was chosen aiming at high-power electronic components based on the working environment and structure characteristics.The thermal design was finished on the research of heat conduction theory for the high-power electronic components.After the finite element model was built,the relations between the thickness and contact area of heat sink and the steady temperature of high-power electronic components were analyzed,and the design of heat sink was optimized.The experimental results showed that the equipment worked well in range of-30~50 ℃ environment,and the steady temperature was less than 85 ℃.Therefore,the equipment of thermal design can satisfy the temperature requirements in the space environment.","PeriodicalId":68706,"journal":{"name":"光机电信息","volume":"28 1","pages":"63-67"},"PeriodicalIF":0.0000,"publicationDate":"2011-01-01","publicationTypes":"Journal Article","fieldsOfStudy":null,"isOpenAccess":false,"openAccessPdf":"","citationCount":"0","resultStr":null,"platform":"Semanticscholar","paperid":null,"PeriodicalName":"光机电信息","FirstCategoryId":"1087","ListUrlMain":"https://doi.org/10.3788/OMEI20112811.0063","RegionNum":0,"RegionCategory":null,"ArticlePicture":[],"TitleCN":null,"AbstractTextCN":null,"PMCID":null,"EPubDate":"","PubModel":"","JCR":"","JCRName":"","Score":null,"Total":0}
引用次数: 0
Abstract
On the research of observation equipment,the method of heat conduction was chosen aiming at high-power electronic components based on the working environment and structure characteristics.The thermal design was finished on the research of heat conduction theory for the high-power electronic components.After the finite element model was built,the relations between the thickness and contact area of heat sink and the steady temperature of high-power electronic components were analyzed,and the design of heat sink was optimized.The experimental results showed that the equipment worked well in range of-30~50 ℃ environment,and the steady temperature was less than 85 ℃.Therefore,the equipment of thermal design can satisfy the temperature requirements in the space environment.