{"title":"电力推进技术与传统推进技术集成的可行性分析","authors":"Shaowei Zhang, Wenzhang Wang","doi":"10.1109/ICMAE52228.2021.9522517","DOIUrl":null,"url":null,"abstract":"This paper introduces the principle and development of Hall thruster and analyzes its own advantages and disadvantages. This paper combines the transition technology which based on traditional chemical thruster with Hall thruster. The ion current with high temperature and high pressure replaces chemical propellant. The ion flow is limited and guided by magnetic field to improve the efficiency of thruster.","PeriodicalId":161846,"journal":{"name":"2021 12th International Conference on Mechanical and Aerospace Engineering (ICMAE)","volume":"23 1","pages":"0"},"PeriodicalIF":0.0000,"publicationDate":"2021-07-16","publicationTypes":"Journal Article","fieldsOfStudy":null,"isOpenAccess":false,"openAccessPdf":"","citationCount":"0","resultStr":"{\"title\":\"Feasibility Analysis of Integration of Electric Propulsion Technology and Traditional Propulsion Technology\",\"authors\":\"Shaowei Zhang, Wenzhang Wang\",\"doi\":\"10.1109/ICMAE52228.2021.9522517\",\"DOIUrl\":null,\"url\":null,\"abstract\":\"This paper introduces the principle and development of Hall thruster and analyzes its own advantages and disadvantages. This paper combines the transition technology which based on traditional chemical thruster with Hall thruster. The ion current with high temperature and high pressure replaces chemical propellant. The ion flow is limited and guided by magnetic field to improve the efficiency of thruster.\",\"PeriodicalId\":161846,\"journal\":{\"name\":\"2021 12th International Conference on Mechanical and Aerospace Engineering (ICMAE)\",\"volume\":\"23 1\",\"pages\":\"0\"},\"PeriodicalIF\":0.0000,\"publicationDate\":\"2021-07-16\",\"publicationTypes\":\"Journal Article\",\"fieldsOfStudy\":null,\"isOpenAccess\":false,\"openAccessPdf\":\"\",\"citationCount\":\"0\",\"resultStr\":null,\"platform\":\"Semanticscholar\",\"paperid\":null,\"PeriodicalName\":\"2021 12th International Conference on Mechanical and Aerospace Engineering (ICMAE)\",\"FirstCategoryId\":\"1085\",\"ListUrlMain\":\"https://doi.org/10.1109/ICMAE52228.2021.9522517\",\"RegionNum\":0,\"RegionCategory\":null,\"ArticlePicture\":[],\"TitleCN\":null,\"AbstractTextCN\":null,\"PMCID\":null,\"EPubDate\":\"\",\"PubModel\":\"\",\"JCR\":\"\",\"JCRName\":\"\",\"Score\":null,\"Total\":0}","platform":"Semanticscholar","paperid":null,"PeriodicalName":"2021 12th International Conference on Mechanical and Aerospace Engineering (ICMAE)","FirstCategoryId":"1085","ListUrlMain":"https://doi.org/10.1109/ICMAE52228.2021.9522517","RegionNum":0,"RegionCategory":null,"ArticlePicture":[],"TitleCN":null,"AbstractTextCN":null,"PMCID":null,"EPubDate":"","PubModel":"","JCR":"","JCRName":"","Score":null,"Total":0}
Feasibility Analysis of Integration of Electric Propulsion Technology and Traditional Propulsion Technology
This paper introduces the principle and development of Hall thruster and analyzes its own advantages and disadvantages. This paper combines the transition technology which based on traditional chemical thruster with Hall thruster. The ion current with high temperature and high pressure replaces chemical propellant. The ion flow is limited and guided by magnetic field to improve the efficiency of thruster.