{"title":"用于电力推进系统推力测量的毫牛顿级推力台的研制","authors":"Ugur Kokal, M. Çelik","doi":"10.1109/RAST.2017.8002970","DOIUrl":null,"url":null,"abstract":"Electric propulsion systems operate with high efficiency, however they generate low thrust. Therefore pendulum based sensitive measurement systems are used for thrust measurements of electric propulsion systems. In this study, a thrust stand is developed and built for the thrust measurements of electric thrusters. The thrust stand that is developed is based on inverted pendulum configuration, and can measure thrust forces at mili-Newton levels with a resolution of ∼100 micro-Newton levels. Measurement range can be changed according to the thruster, by adjusting the components of the thrust stand.","PeriodicalId":434418,"journal":{"name":"2017 8th International Conference on Recent Advances in Space Technologies (RAST)","volume":"7 1","pages":"0"},"PeriodicalIF":0.0000,"publicationDate":"1900-01-01","publicationTypes":"Journal Article","fieldsOfStudy":null,"isOpenAccess":false,"openAccessPdf":"","citationCount":"10","resultStr":"{\"title\":\"Development of a mili-Newton level thrust stand for thrust measurements of electric propulsion systems\",\"authors\":\"Ugur Kokal, M. Çelik\",\"doi\":\"10.1109/RAST.2017.8002970\",\"DOIUrl\":null,\"url\":null,\"abstract\":\"Electric propulsion systems operate with high efficiency, however they generate low thrust. Therefore pendulum based sensitive measurement systems are used for thrust measurements of electric propulsion systems. In this study, a thrust stand is developed and built for the thrust measurements of electric thrusters. The thrust stand that is developed is based on inverted pendulum configuration, and can measure thrust forces at mili-Newton levels with a resolution of ∼100 micro-Newton levels. Measurement range can be changed according to the thruster, by adjusting the components of the thrust stand.\",\"PeriodicalId\":434418,\"journal\":{\"name\":\"2017 8th International Conference on Recent Advances in Space Technologies (RAST)\",\"volume\":\"7 1\",\"pages\":\"0\"},\"PeriodicalIF\":0.0000,\"publicationDate\":\"1900-01-01\",\"publicationTypes\":\"Journal Article\",\"fieldsOfStudy\":null,\"isOpenAccess\":false,\"openAccessPdf\":\"\",\"citationCount\":\"10\",\"resultStr\":null,\"platform\":\"Semanticscholar\",\"paperid\":null,\"PeriodicalName\":\"2017 8th International Conference on Recent Advances in Space Technologies (RAST)\",\"FirstCategoryId\":\"1085\",\"ListUrlMain\":\"https://doi.org/10.1109/RAST.2017.8002970\",\"RegionNum\":0,\"RegionCategory\":null,\"ArticlePicture\":[],\"TitleCN\":null,\"AbstractTextCN\":null,\"PMCID\":null,\"EPubDate\":\"\",\"PubModel\":\"\",\"JCR\":\"\",\"JCRName\":\"\",\"Score\":null,\"Total\":0}","platform":"Semanticscholar","paperid":null,"PeriodicalName":"2017 8th International Conference on Recent Advances in Space Technologies (RAST)","FirstCategoryId":"1085","ListUrlMain":"https://doi.org/10.1109/RAST.2017.8002970","RegionNum":0,"RegionCategory":null,"ArticlePicture":[],"TitleCN":null,"AbstractTextCN":null,"PMCID":null,"EPubDate":"","PubModel":"","JCR":"","JCRName":"","Score":null,"Total":0}
Development of a mili-Newton level thrust stand for thrust measurements of electric propulsion systems
Electric propulsion systems operate with high efficiency, however they generate low thrust. Therefore pendulum based sensitive measurement systems are used for thrust measurements of electric propulsion systems. In this study, a thrust stand is developed and built for the thrust measurements of electric thrusters. The thrust stand that is developed is based on inverted pendulum configuration, and can measure thrust forces at mili-Newton levels with a resolution of ∼100 micro-Newton levels. Measurement range can be changed according to the thruster, by adjusting the components of the thrust stand.