{"title":"汽化水微型推进器","authors":"X. Ye, F. Tang, Haiqing Ding, Zhaoying Zhou","doi":"10.1109/MEMSYS.2000.838493","DOIUrl":null,"url":null,"abstract":"Vaporizing water micro-thrusters are fabricated and tested. A single micro-thruster we developed, fabricated by MEMS technologies, consists of a microresistor, a vaporizing chamber, a nozzle, a propellant inlet and a micro channel. The water propellant is fed into the thruster from a propellant tank by capillary force and pressure. The micro-thruster works in a pulse mode. During each period, an electric pulse is applied on the micro-resistor to heat the water in the chamber to vaporize it into high-pressure gas. A thrust is then produced as the gas exits through the nozzle. Test results show that for a single micro-thruster with pulse power of 48 W, the total impulse produced in a second is more than 0.2/spl times/10/sup -6/ N/spl middot/s.","PeriodicalId":251857,"journal":{"name":"Proceedings IEEE Thirteenth Annual International Conference on Micro Electro Mechanical Systems (Cat. No.00CH36308)","volume":"95 1","pages":"0"},"PeriodicalIF":0.0000,"publicationDate":"2000-01-23","publicationTypes":"Journal Article","fieldsOfStudy":null,"isOpenAccess":false,"openAccessPdf":"","citationCount":"10","resultStr":"{\"title\":\"A vaporizing water micro-thruster\",\"authors\":\"X. Ye, F. Tang, Haiqing Ding, Zhaoying Zhou\",\"doi\":\"10.1109/MEMSYS.2000.838493\",\"DOIUrl\":null,\"url\":null,\"abstract\":\"Vaporizing water micro-thrusters are fabricated and tested. A single micro-thruster we developed, fabricated by MEMS technologies, consists of a microresistor, a vaporizing chamber, a nozzle, a propellant inlet and a micro channel. The water propellant is fed into the thruster from a propellant tank by capillary force and pressure. The micro-thruster works in a pulse mode. During each period, an electric pulse is applied on the micro-resistor to heat the water in the chamber to vaporize it into high-pressure gas. A thrust is then produced as the gas exits through the nozzle. Test results show that for a single micro-thruster with pulse power of 48 W, the total impulse produced in a second is more than 0.2/spl times/10/sup -6/ N/spl middot/s.\",\"PeriodicalId\":251857,\"journal\":{\"name\":\"Proceedings IEEE Thirteenth Annual International Conference on Micro Electro Mechanical Systems (Cat. No.00CH36308)\",\"volume\":\"95 1\",\"pages\":\"0\"},\"PeriodicalIF\":0.0000,\"publicationDate\":\"2000-01-23\",\"publicationTypes\":\"Journal Article\",\"fieldsOfStudy\":null,\"isOpenAccess\":false,\"openAccessPdf\":\"\",\"citationCount\":\"10\",\"resultStr\":null,\"platform\":\"Semanticscholar\",\"paperid\":null,\"PeriodicalName\":\"Proceedings IEEE Thirteenth Annual International Conference on Micro Electro Mechanical Systems (Cat. No.00CH36308)\",\"FirstCategoryId\":\"1085\",\"ListUrlMain\":\"https://doi.org/10.1109/MEMSYS.2000.838493\",\"RegionNum\":0,\"RegionCategory\":null,\"ArticlePicture\":[],\"TitleCN\":null,\"AbstractTextCN\":null,\"PMCID\":null,\"EPubDate\":\"\",\"PubModel\":\"\",\"JCR\":\"\",\"JCRName\":\"\",\"Score\":null,\"Total\":0}","platform":"Semanticscholar","paperid":null,"PeriodicalName":"Proceedings IEEE Thirteenth Annual International Conference on Micro Electro Mechanical Systems (Cat. No.00CH36308)","FirstCategoryId":"1085","ListUrlMain":"https://doi.org/10.1109/MEMSYS.2000.838493","RegionNum":0,"RegionCategory":null,"ArticlePicture":[],"TitleCN":null,"AbstractTextCN":null,"PMCID":null,"EPubDate":"","PubModel":"","JCR":"","JCRName":"","Score":null,"Total":0}
Vaporizing water micro-thrusters are fabricated and tested. A single micro-thruster we developed, fabricated by MEMS technologies, consists of a microresistor, a vaporizing chamber, a nozzle, a propellant inlet and a micro channel. The water propellant is fed into the thruster from a propellant tank by capillary force and pressure. The micro-thruster works in a pulse mode. During each period, an electric pulse is applied on the micro-resistor to heat the water in the chamber to vaporize it into high-pressure gas. A thrust is then produced as the gas exits through the nozzle. Test results show that for a single micro-thruster with pulse power of 48 W, the total impulse produced in a second is more than 0.2/spl times/10/sup -6/ N/spl middot/s.