{"title":"铁电微等离子体推力器输出电流的测量","authors":"Hai Wang, Biao Yang, Yang Any, L. Wen","doi":"10.1109/NEMS.2016.7758212","DOIUrl":null,"url":null,"abstract":"Electrical microthruster have been widely applied in micro and nano-satellites, dute to its light weight and low cost. A microthruster based on ferroelectrical plasma is developed to realized microscale Newton thrust applications. Measurement of thrust generated from the ferroelectric miro-plasma thruster(FMPT) is crtical for the design of FMPT. A charge collector based on capacitor charging principle is proposed to measure the ion current from the nozzle of the ferroelectric micro-plasma thruster(FMPT).","PeriodicalId":150449,"journal":{"name":"2016 IEEE 11th Annual International Conference on Nano/Micro Engineered and Molecular Systems (NEMS)","volume":"148 1","pages":"0"},"PeriodicalIF":0.0000,"publicationDate":"2016-04-01","publicationTypes":"Journal Article","fieldsOfStudy":null,"isOpenAccess":false,"openAccessPdf":"","citationCount":"1","resultStr":"{\"title\":\"Measurement of output current for ferroelectric micro-plasma thruster\",\"authors\":\"Hai Wang, Biao Yang, Yang Any, L. Wen\",\"doi\":\"10.1109/NEMS.2016.7758212\",\"DOIUrl\":null,\"url\":null,\"abstract\":\"Electrical microthruster have been widely applied in micro and nano-satellites, dute to its light weight and low cost. A microthruster based on ferroelectrical plasma is developed to realized microscale Newton thrust applications. Measurement of thrust generated from the ferroelectric miro-plasma thruster(FMPT) is crtical for the design of FMPT. A charge collector based on capacitor charging principle is proposed to measure the ion current from the nozzle of the ferroelectric micro-plasma thruster(FMPT).\",\"PeriodicalId\":150449,\"journal\":{\"name\":\"2016 IEEE 11th Annual International Conference on Nano/Micro Engineered and Molecular Systems (NEMS)\",\"volume\":\"148 1\",\"pages\":\"0\"},\"PeriodicalIF\":0.0000,\"publicationDate\":\"2016-04-01\",\"publicationTypes\":\"Journal Article\",\"fieldsOfStudy\":null,\"isOpenAccess\":false,\"openAccessPdf\":\"\",\"citationCount\":\"1\",\"resultStr\":null,\"platform\":\"Semanticscholar\",\"paperid\":null,\"PeriodicalName\":\"2016 IEEE 11th Annual International Conference on Nano/Micro Engineered and Molecular Systems (NEMS)\",\"FirstCategoryId\":\"1085\",\"ListUrlMain\":\"https://doi.org/10.1109/NEMS.2016.7758212\",\"RegionNum\":0,\"RegionCategory\":null,\"ArticlePicture\":[],\"TitleCN\":null,\"AbstractTextCN\":null,\"PMCID\":null,\"EPubDate\":\"\",\"PubModel\":\"\",\"JCR\":\"\",\"JCRName\":\"\",\"Score\":null,\"Total\":0}","platform":"Semanticscholar","paperid":null,"PeriodicalName":"2016 IEEE 11th Annual International Conference on Nano/Micro Engineered and Molecular Systems (NEMS)","FirstCategoryId":"1085","ListUrlMain":"https://doi.org/10.1109/NEMS.2016.7758212","RegionNum":0,"RegionCategory":null,"ArticlePicture":[],"TitleCN":null,"AbstractTextCN":null,"PMCID":null,"EPubDate":"","PubModel":"","JCR":"","JCRName":"","Score":null,"Total":0}
Measurement of output current for ferroelectric micro-plasma thruster
Electrical microthruster have been widely applied in micro and nano-satellites, dute to its light weight and low cost. A microthruster based on ferroelectrical plasma is developed to realized microscale Newton thrust applications. Measurement of thrust generated from the ferroelectric miro-plasma thruster(FMPT) is crtical for the design of FMPT. A charge collector based on capacitor charging principle is proposed to measure the ion current from the nozzle of the ferroelectric micro-plasma thruster(FMPT).
京公网安备 11010802042870号
京ICP备2023020795号-1
分享
求助内容：
应助结果提醒方式：
扫码关注我们
