{"title":"航天飞机轨道器电力系统中的线路可更换单元分析","authors":"T. Oepomo","doi":"10.1109/TPAS.1985.318902","DOIUrl":null,"url":null,"abstract":"The National Aeronautics and Space Administration (NASA) Space Shuttle orbiter, as a test bed for low-orbit space laboratory experiments, needs an orbiter voltage analysis on all orbiter line replaceable units (LRU's). This analysis should use a mathematical model to predict voltages at the various LRU's so that voltage drops from a bus to an LRU can then be computed based on calculated resistance of the conductors and load current.","PeriodicalId":227345,"journal":{"name":"IEEE Transactions on Power Apparatus and Systems","volume":"1 1","pages":"0"},"PeriodicalIF":0.0000,"publicationDate":"1985-12-01","publicationTypes":"Journal Article","fieldsOfStudy":null,"isOpenAccess":false,"openAccessPdf":"","citationCount":"0","resultStr":"{\"title\":\"Line Replaceable Unit (LRU) Analysis in the Space Shuttle Orbiter Electrical Power System\",\"authors\":\"T. Oepomo\",\"doi\":\"10.1109/TPAS.1985.318902\",\"DOIUrl\":null,\"url\":null,\"abstract\":\"The National Aeronautics and Space Administration (NASA) Space Shuttle orbiter, as a test bed for low-orbit space laboratory experiments, needs an orbiter voltage analysis on all orbiter line replaceable units (LRU's). This analysis should use a mathematical model to predict voltages at the various LRU's so that voltage drops from a bus to an LRU can then be computed based on calculated resistance of the conductors and load current.\",\"PeriodicalId\":227345,\"journal\":{\"name\":\"IEEE Transactions on Power Apparatus and Systems\",\"volume\":\"1 1\",\"pages\":\"0\"},\"PeriodicalIF\":0.0000,\"publicationDate\":\"1985-12-01\",\"publicationTypes\":\"Journal Article\",\"fieldsOfStudy\":null,\"isOpenAccess\":false,\"openAccessPdf\":\"\",\"citationCount\":\"0\",\"resultStr\":null,\"platform\":\"Semanticscholar\",\"paperid\":null,\"PeriodicalName\":\"IEEE Transactions on Power Apparatus and Systems\",\"FirstCategoryId\":\"1085\",\"ListUrlMain\":\"https://doi.org/10.1109/TPAS.1985.318902\",\"RegionNum\":0,\"RegionCategory\":null,\"ArticlePicture\":[],\"TitleCN\":null,\"AbstractTextCN\":null,\"PMCID\":null,\"EPubDate\":\"\",\"PubModel\":\"\",\"JCR\":\"\",\"JCRName\":\"\",\"Score\":null,\"Total\":0}","platform":"Semanticscholar","paperid":null,"PeriodicalName":"IEEE Transactions on Power Apparatus and Systems","FirstCategoryId":"1085","ListUrlMain":"https://doi.org/10.1109/TPAS.1985.318902","RegionNum":0,"RegionCategory":null,"ArticlePicture":[],"TitleCN":null,"AbstractTextCN":null,"PMCID":null,"EPubDate":"","PubModel":"","JCR":"","JCRName":"","Score":null,"Total":0}
Line Replaceable Unit (LRU) Analysis in the Space Shuttle Orbiter Electrical Power System
The National Aeronautics and Space Administration (NASA) Space Shuttle orbiter, as a test bed for low-orbit space laboratory experiments, needs an orbiter voltage analysis on all orbiter line replaceable units (LRU's). This analysis should use a mathematical model to predict voltages at the various LRU's so that voltage drops from a bus to an LRU can then be computed based on calculated resistance of the conductors and load current.