Collin Whittaker, Steven Arestie, Colleen Marrese-Reading, Benjamin Jorns
{"title":"10w级电喷雾阵列推进器的特性研究。","authors":"Collin Whittaker, Steven Arestie, Colleen Marrese-Reading, Benjamin Jorns","doi":"10.1007/s44205-025-00114-4","DOIUrl":null,"url":null,"abstract":"<p><p>A porous conical type electrospray array thruster consisting of 6102 individual emitters is operated at up to 13.3 W power. The design and manufacture of the thruster are described, including its porous glass emitter chip and metallized ceramic extractor chip. A precision mass balance mounted inside a bell jar is used to directly measure the thrust, specific impulse, and efficiency in negative polarity, from <math><mrow><mn>42</mn> <mo>±</mo> <mn>0.5</mn> <mspace></mspace> <mi>μ</mi></mrow> </math> N, <math><mrow><mn>1050</mn> <mo>±</mo> <mn>26</mn></mrow> </math> s, and <math><mrow><mn>57</mn> <mo>±</mo> <mn>1.9</mn></mrow> </math> % at <math><mrow><mo>-</mo> <mn>1000</mn></mrow> </math> V and 0.38 W to <math><mrow><mn>174</mn> <mo>±</mo> <mn>0.5</mn> <mspace></mspace> <mi>μ</mi></mrow> </math> N, <math><mrow><mn>420</mn> <mo>±</mo> <mn>2</mn></mrow> </math> s, and <math><mrow><mn>21</mn> <mo>±</mo> <mn>0.3</mn></mrow> </math> % at <math><mrow><mo>-</mo> <mn>1300</mn></mrow> </math> V and 1.7 W. Additional negative polarity experiments in a 2 meter vacuum facility demonstrate powers from order 1 <math><mi>μ</mi></math> W to over 10 W, spanning 7 orders of magnitude. Power and performance measurements were not repeated for positive mode operation, as this was found to induce arcing between the emitter and extractor electrodes at 1400 V and above. The drop in efficiency from <math><mrow><mo>-</mo> <mn>1000</mn></mrow> </math> V to <math><mrow><mo>-</mo> <mn>1300</mn></mrow> </math> V operation in the bell jar is discussed within the context of facility effects, and secondary charged particle flux to the thruster is identified as a likely contributor. Finally, the performance of the thruster is considered relative to scaling electrospray systems to higher power robustly.</p><p><strong>Supplementary information: </strong>The online version contains supplementary material available at 10.1007/s44205-025-00114-4.</p>","PeriodicalId":73724,"journal":{"name":"Journal of electric propulsion","volume":"4 1","pages":"20"},"PeriodicalIF":0.0000,"publicationDate":"2025-01-01","publicationTypes":"Journal Article","fieldsOfStudy":null,"isOpenAccess":false,"openAccessPdf":"https://www.ncbi.nlm.nih.gov/pmc/articles/PMC11947065/pdf/","citationCount":"0","resultStr":"{\"title\":\"Characterization of a 10 W class electrospray array thruster.\",\"authors\":\"Collin Whittaker, Steven Arestie, Colleen Marrese-Reading, Benjamin Jorns\",\"doi\":\"10.1007/s44205-025-00114-4\",\"DOIUrl\":null,\"url\":null,\"abstract\":\"<p><p>A porous conical type electrospray array thruster consisting of 6102 individual emitters is operated at up to 13.3 W power. The design and manufacture of the thruster are described, including its porous glass emitter chip and metallized ceramic extractor chip. A precision mass balance mounted inside a bell jar is used to directly measure the thrust, specific impulse, and efficiency in negative polarity, from <math><mrow><mn>42</mn> <mo>±</mo> <mn>0.5</mn> <mspace></mspace> <mi>μ</mi></mrow> </math> N, <math><mrow><mn>1050</mn> <mo>±</mo> <mn>26</mn></mrow> </math> s, and <math><mrow><mn>57</mn> <mo>±</mo> <mn>1.9</mn></mrow> </math> % at <math><mrow><mo>-</mo> <mn>1000</mn></mrow> </math> V and 0.38 W to <math><mrow><mn>174</mn> <mo>±</mo> <mn>0.5</mn> <mspace></mspace> <mi>μ</mi></mrow> </math> N, <math><mrow><mn>420</mn> <mo>±</mo> <mn>2</mn></mrow> </math> s, and <math><mrow><mn>21</mn> <mo>±</mo> <mn>0.3</mn></mrow> </math> % at <math><mrow><mo>-</mo> <mn>1300</mn></mrow> </math> V and 1.7 W. Additional negative polarity experiments in a 2 meter vacuum facility demonstrate powers from order 1 <math><mi>μ</mi></math> W to over 10 W, spanning 7 orders of magnitude. Power and performance measurements were not repeated for positive mode operation, as this was found to induce arcing between the emitter and extractor electrodes at 1400 V and above. The drop in efficiency from <math><mrow><mo>-</mo> <mn>1000</mn></mrow> </math> V to <math><mrow><mo>-</mo> <mn>1300</mn></mrow> </math> V operation in the bell jar is discussed within the context of facility effects, and secondary charged particle flux to the thruster is identified as a likely contributor. Finally, the performance of the thruster is considered relative to scaling electrospray systems to higher power robustly.</p><p><strong>Supplementary information: </strong>The online version contains supplementary material available at 10.1007/s44205-025-00114-4.</p>\",\"PeriodicalId\":73724,\"journal\":{\"name\":\"Journal of electric propulsion\",\"volume\":\"4 1\",\"pages\":\"20\"},\"PeriodicalIF\":0.0000,\"publicationDate\":\"2025-01-01\",\"publicationTypes\":\"Journal Article\",\"fieldsOfStudy\":null,\"isOpenAccess\":false,\"openAccessPdf\":\"https://www.ncbi.nlm.nih.gov/pmc/articles/PMC11947065/pdf/\",\"citationCount\":\"0\",\"resultStr\":null,\"platform\":\"Semanticscholar\",\"paperid\":null,\"PeriodicalName\":\"Journal of electric propulsion\",\"FirstCategoryId\":\"1085\",\"ListUrlMain\":\"https://doi.org/10.1007/s44205-025-00114-4\",\"RegionNum\":0,\"RegionCategory\":null,\"ArticlePicture\":[],\"TitleCN\":null,\"AbstractTextCN\":null,\"PMCID\":null,\"EPubDate\":\"2025/3/26 0:00:00\",\"PubModel\":\"Epub\",\"JCR\":\"\",\"JCRName\":\"\",\"Score\":null,\"Total\":0}","platform":"Semanticscholar","paperid":null,"PeriodicalName":"Journal of electric propulsion","FirstCategoryId":"1085","ListUrlMain":"https://doi.org/10.1007/s44205-025-00114-4","RegionNum":0,"RegionCategory":null,"ArticlePicture":[],"TitleCN":null,"AbstractTextCN":null,"PMCID":null,"EPubDate":"2025/3/26 0:00:00","PubModel":"Epub","JCR":"","JCRName":"","Score":null,"Total":0}
Characterization of a 10 W class electrospray array thruster.
A porous conical type electrospray array thruster consisting of 6102 individual emitters is operated at up to 13.3 W power. The design and manufacture of the thruster are described, including its porous glass emitter chip and metallized ceramic extractor chip. A precision mass balance mounted inside a bell jar is used to directly measure the thrust, specific impulse, and efficiency in negative polarity, from N, s, and % at V and 0.38 W to N, s, and % at V and 1.7 W. Additional negative polarity experiments in a 2 meter vacuum facility demonstrate powers from order 1 W to over 10 W, spanning 7 orders of magnitude. Power and performance measurements were not repeated for positive mode operation, as this was found to induce arcing between the emitter and extractor electrodes at 1400 V and above. The drop in efficiency from V to V operation in the bell jar is discussed within the context of facility effects, and secondary charged particle flux to the thruster is identified as a likely contributor. Finally, the performance of the thruster is considered relative to scaling electrospray systems to higher power robustly.
Supplementary information: The online version contains supplementary material available at 10.1007/s44205-025-00114-4.