{"title":"航天器单相热控系统的数学建模","authors":"A. Delcov, A. Hodenkov, D. A. Zhuikov","doi":"10.1109/APEIE.2014.7040754","DOIUrl":null,"url":null,"abstract":"This article discusses the modeling of heat transfer in elementary contour-phase thermal control system. Calculated relations to characterize the circuit are given. Results of calculation are described. Problems and prospects of mathematical modeling of systems of spacecraft thermal control are evaluated.","PeriodicalId":202524,"journal":{"name":"2014 12th International Conference on Actual Problems of Electronics Instrument Engineering (APEIE)","volume":"52 1","pages":"0"},"PeriodicalIF":0.0000,"publicationDate":"2014-10-01","publicationTypes":"Journal Article","fieldsOfStudy":null,"isOpenAccess":false,"openAccessPdf":"","citationCount":"0","resultStr":"{\"title\":\"Mathematical modeling of single-phase thermal control system of the spacecraft\",\"authors\":\"A. Delcov, A. Hodenkov, D. A. Zhuikov\",\"doi\":\"10.1109/APEIE.2014.7040754\",\"DOIUrl\":null,\"url\":null,\"abstract\":\"This article discusses the modeling of heat transfer in elementary contour-phase thermal control system. Calculated relations to characterize the circuit are given. Results of calculation are described. Problems and prospects of mathematical modeling of systems of spacecraft thermal control are evaluated.\",\"PeriodicalId\":202524,\"journal\":{\"name\":\"2014 12th International Conference on Actual Problems of Electronics Instrument Engineering (APEIE)\",\"volume\":\"52 1\",\"pages\":\"0\"},\"PeriodicalIF\":0.0000,\"publicationDate\":\"2014-10-01\",\"publicationTypes\":\"Journal Article\",\"fieldsOfStudy\":null,\"isOpenAccess\":false,\"openAccessPdf\":\"\",\"citationCount\":\"0\",\"resultStr\":null,\"platform\":\"Semanticscholar\",\"paperid\":null,\"PeriodicalName\":\"2014 12th International Conference on Actual Problems of Electronics Instrument Engineering (APEIE)\",\"FirstCategoryId\":\"1085\",\"ListUrlMain\":\"https://doi.org/10.1109/APEIE.2014.7040754\",\"RegionNum\":0,\"RegionCategory\":null,\"ArticlePicture\":[],\"TitleCN\":null,\"AbstractTextCN\":null,\"PMCID\":null,\"EPubDate\":\"\",\"PubModel\":\"\",\"JCR\":\"\",\"JCRName\":\"\",\"Score\":null,\"Total\":0}","platform":"Semanticscholar","paperid":null,"PeriodicalName":"2014 12th International Conference on Actual Problems of Electronics Instrument Engineering (APEIE)","FirstCategoryId":"1085","ListUrlMain":"https://doi.org/10.1109/APEIE.2014.7040754","RegionNum":0,"RegionCategory":null,"ArticlePicture":[],"TitleCN":null,"AbstractTextCN":null,"PMCID":null,"EPubDate":"","PubModel":"","JCR":"","JCRName":"","Score":null,"Total":0}
Mathematical modeling of single-phase thermal control system of the spacecraft
This article discusses the modeling of heat transfer in elementary contour-phase thermal control system. Calculated relations to characterize the circuit are given. Results of calculation are described. Problems and prospects of mathematical modeling of systems of spacecraft thermal control are evaluated.
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