{"title":"微型卫星用高温超导磁体动量轮","authors":"Eunjeong Lee, Jang-Horng Yu, T. L. Wilson","doi":"10.1109/AERO.2001.931207","DOIUrl":null,"url":null,"abstract":"We have constructed a superconductor-magnet momentum wheel, which is based on passive magnetic levitation and the flux pinning effect of high-temperature superconductivity. The high-temperature superconductor (HTS) flywheel has high angular momentum storage capacity because its drag torque is essentially velocity-independent and extremely small, enabling high-speed rotation. It has mass of 1.1 kg with an angular momentum capacity of 3.5 J sec. It occupies a volume of 12.7 cm in diameter and 5 cm in height. It operates within the restricted power budget of a micro satellite with a total power supply of 10 W only. It consumes less than 1 W for sustenance. While there exist momentum wheels comparable to ours in one respect, there is none better than ours in all respects of angular momentum storage, volume and low power consumption.","PeriodicalId":329225,"journal":{"name":"2001 IEEE Aerospace Conference Proceedings (Cat. No.01TH8542)","volume":"477 1","pages":"0"},"PeriodicalIF":0.0000,"publicationDate":"2001-03-10","publicationTypes":"Journal Article","fieldsOfStudy":null,"isOpenAccess":false,"openAccessPdf":"","citationCount":"2","resultStr":"{\"title\":\"High-temperature superconductor-magnet momentum wheel for micro satellite\",\"authors\":\"Eunjeong Lee, Jang-Horng Yu, T. L. Wilson\",\"doi\":\"10.1109/AERO.2001.931207\",\"DOIUrl\":null,\"url\":null,\"abstract\":\"We have constructed a superconductor-magnet momentum wheel, which is based on passive magnetic levitation and the flux pinning effect of high-temperature superconductivity. The high-temperature superconductor (HTS) flywheel has high angular momentum storage capacity because its drag torque is essentially velocity-independent and extremely small, enabling high-speed rotation. It has mass of 1.1 kg with an angular momentum capacity of 3.5 J sec. It occupies a volume of 12.7 cm in diameter and 5 cm in height. It operates within the restricted power budget of a micro satellite with a total power supply of 10 W only. It consumes less than 1 W for sustenance. While there exist momentum wheels comparable to ours in one respect, there is none better than ours in all respects of angular momentum storage, volume and low power consumption.\",\"PeriodicalId\":329225,\"journal\":{\"name\":\"2001 IEEE Aerospace Conference Proceedings (Cat. No.01TH8542)\",\"volume\":\"477 1\",\"pages\":\"0\"},\"PeriodicalIF\":0.0000,\"publicationDate\":\"2001-03-10\",\"publicationTypes\":\"Journal Article\",\"fieldsOfStudy\":null,\"isOpenAccess\":false,\"openAccessPdf\":\"\",\"citationCount\":\"2\",\"resultStr\":null,\"platform\":\"Semanticscholar\",\"paperid\":null,\"PeriodicalName\":\"2001 IEEE Aerospace Conference Proceedings (Cat. No.01TH8542)\",\"FirstCategoryId\":\"1085\",\"ListUrlMain\":\"https://doi.org/10.1109/AERO.2001.931207\",\"RegionNum\":0,\"RegionCategory\":null,\"ArticlePicture\":[],\"TitleCN\":null,\"AbstractTextCN\":null,\"PMCID\":null,\"EPubDate\":\"\",\"PubModel\":\"\",\"JCR\":\"\",\"JCRName\":\"\",\"Score\":null,\"Total\":0}","platform":"Semanticscholar","paperid":null,"PeriodicalName":"2001 IEEE Aerospace Conference Proceedings (Cat. No.01TH8542)","FirstCategoryId":"1085","ListUrlMain":"https://doi.org/10.1109/AERO.2001.931207","RegionNum":0,"RegionCategory":null,"ArticlePicture":[],"TitleCN":null,"AbstractTextCN":null,"PMCID":null,"EPubDate":"","PubModel":"","JCR":"","JCRName":"","Score":null,"Total":0}
High-temperature superconductor-magnet momentum wheel for micro satellite
We have constructed a superconductor-magnet momentum wheel, which is based on passive magnetic levitation and the flux pinning effect of high-temperature superconductivity. The high-temperature superconductor (HTS) flywheel has high angular momentum storage capacity because its drag torque is essentially velocity-independent and extremely small, enabling high-speed rotation. It has mass of 1.1 kg with an angular momentum capacity of 3.5 J sec. It occupies a volume of 12.7 cm in diameter and 5 cm in height. It operates within the restricted power budget of a micro satellite with a total power supply of 10 W only. It consumes less than 1 W for sustenance. While there exist momentum wheels comparable to ours in one respect, there is none better than ours in all respects of angular momentum storage, volume and low power consumption.
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