{"title":"LaB6干阴极与水蒸汽霍尔效应推力器耦合的性能特性","authors":"Daigo Takasaki , Aoma Fujimori , Hiroyuki Koizumi , Hokuto Sekine , Isami Dainichi , Kimiya Komurasaki","doi":"10.1016/j.actaastro.2025.08.032","DOIUrl":null,"url":null,"abstract":"<div><div>In this study, a lanthanum hexaboride (LaB<span><math><msub><mrow></mrow><mrow><mn>6</mn></mrow></msub></math></span>) dry cathode was tested in both diode mode with a graphite collector plate and coupling mode with a plume of a water-vapor Hall effect thruster (HET), in order to evaluate its compatibility. The work function of polycrystalline LaB<span><math><msub><mrow></mrow><mrow><mn>6</mn></mrow></msub></math></span>, initially 3.06 eV in diode mode, increased to approximately 3.6 ± 0.2 eV in coupling mode. This shift was consistent with post-operation oxygen deposition on the emitter surface, as revealed by energy-dispersive X-ray spectroscopy. The cathode emitted 200 mA of electron current with 100 V of negative bias voltage in the coupling configuration and it was roughly ten times higher than the space-charge-limited current observed in diode mode. Fitting equations were developed based on experimental data to predict the dry cathode performance under a broader range of operational conditions. Calculations indicated that electron production cost could be less than 150 W/A, surpassing that of a water radio frequency (RF) cathode. The estimated emitter erosion rate was below <span><math><mrow><mn>8</mn><mo>×</mo><mn>1</mn><msup><mrow><mn>0</mn></mrow><mrow><mo>−</mo><mn>3</mn></mrow></msup><mspace></mspace><mi>mm/h</mi></mrow></math></span>, suggesting sufficient lifetime for HET operation. The thruster efficiency of a water-vapor HET employing the LaB<span><math><msub><mrow></mrow><mrow><mn>6</mn></mrow></msub></math></span> dry cathode was estimated to reach 9.7% at a discharge voltage of 350 V and an anode mass flow rate of 0.68 mg/s, comparable to that of a xenon RF cathode. These results highlight the strong potential of LaB<span><math><msub><mrow></mrow><mrow><mn>6</mn></mrow></msub></math></span> dry cathodes for use in water-vapor HETs.</div></div>","PeriodicalId":44971,"journal":{"name":"Acta Astronautica","volume":"237 ","pages":"Pages 208-223"},"PeriodicalIF":3.4000,"publicationDate":"2025-08-22","publicationTypes":"Journal Article","fieldsOfStudy":null,"isOpenAccess":false,"openAccessPdf":"","citationCount":"0","resultStr":"{\"title\":\"Performance characteristics of a LaB6 dry cathode coupled with a water-vapor Hall effect thruster\",\"authors\":\"Daigo Takasaki , Aoma Fujimori , Hiroyuki Koizumi , Hokuto Sekine , Isami Dainichi , Kimiya Komurasaki\",\"doi\":\"10.1016/j.actaastro.2025.08.032\",\"DOIUrl\":null,\"url\":null,\"abstract\":\"<div><div>In this study, a lanthanum hexaboride (LaB<span><math><msub><mrow></mrow><mrow><mn>6</mn></mrow></msub></math></span>) dry cathode was tested in both diode mode with a graphite collector plate and coupling mode with a plume of a water-vapor Hall effect thruster (HET), in order to evaluate its compatibility. The work function of polycrystalline LaB<span><math><msub><mrow></mrow><mrow><mn>6</mn></mrow></msub></math></span>, initially 3.06 eV in diode mode, increased to approximately 3.6 ± 0.2 eV in coupling mode. This shift was consistent with post-operation oxygen deposition on the emitter surface, as revealed by energy-dispersive X-ray spectroscopy. The cathode emitted 200 mA of electron current with 100 V of negative bias voltage in the coupling configuration and it was roughly ten times higher than the space-charge-limited current observed in diode mode. Fitting equations were developed based on experimental data to predict the dry cathode performance under a broader range of operational conditions. Calculations indicated that electron production cost could be less than 150 W/A, surpassing that of a water radio frequency (RF) cathode. The estimated emitter erosion rate was below <span><math><mrow><mn>8</mn><mo>×</mo><mn>1</mn><msup><mrow><mn>0</mn></mrow><mrow><mo>−</mo><mn>3</mn></mrow></msup><mspace></mspace><mi>mm/h</mi></mrow></math></span>, suggesting sufficient lifetime for HET operation. The thruster efficiency of a water-vapor HET employing the LaB<span><math><msub><mrow></mrow><mrow><mn>6</mn></mrow></msub></math></span> dry cathode was estimated to reach 9.7% at a discharge voltage of 350 V and an anode mass flow rate of 0.68 mg/s, comparable to that of a xenon RF cathode. These results highlight the strong potential of LaB<span><math><msub><mrow></mrow><mrow><mn>6</mn></mrow></msub></math></span> dry cathodes for use in water-vapor HETs.</div></div>\",\"PeriodicalId\":44971,\"journal\":{\"name\":\"Acta Astronautica\",\"volume\":\"237 \",\"pages\":\"Pages 208-223\"},\"PeriodicalIF\":3.4000,\"publicationDate\":\"2025-08-22\",\"publicationTypes\":\"Journal Article\",\"fieldsOfStudy\":null,\"isOpenAccess\":false,\"openAccessPdf\":\"\",\"citationCount\":\"0\",\"resultStr\":null,\"platform\":\"Semanticscholar\",\"paperid\":null,\"PeriodicalName\":\"Acta Astronautica\",\"FirstCategoryId\":\"5\",\"ListUrlMain\":\"https://www.sciencedirect.com/science/article/pii/S0094576525005338\",\"RegionNum\":2,\"RegionCategory\":\"物理与天体物理\",\"ArticlePicture\":[],\"TitleCN\":null,\"AbstractTextCN\":null,\"PMCID\":null,\"EPubDate\":\"\",\"PubModel\":\"\",\"JCR\":\"Q1\",\"JCRName\":\"ENGINEERING, AEROSPACE\",\"Score\":null,\"Total\":0}","platform":"Semanticscholar","paperid":null,"PeriodicalName":"Acta Astronautica","FirstCategoryId":"5","ListUrlMain":"https://www.sciencedirect.com/science/article/pii/S0094576525005338","RegionNum":2,"RegionCategory":"物理与天体物理","ArticlePicture":[],"TitleCN":null,"AbstractTextCN":null,"PMCID":null,"EPubDate":"","PubModel":"","JCR":"Q1","JCRName":"ENGINEERING, AEROSPACE","Score":null,"Total":0}
Performance characteristics of a LaB6 dry cathode coupled with a water-vapor Hall effect thruster
In this study, a lanthanum hexaboride (LaB) dry cathode was tested in both diode mode with a graphite collector plate and coupling mode with a plume of a water-vapor Hall effect thruster (HET), in order to evaluate its compatibility. The work function of polycrystalline LaB, initially 3.06 eV in diode mode, increased to approximately 3.6 ± 0.2 eV in coupling mode. This shift was consistent with post-operation oxygen deposition on the emitter surface, as revealed by energy-dispersive X-ray spectroscopy. The cathode emitted 200 mA of electron current with 100 V of negative bias voltage in the coupling configuration and it was roughly ten times higher than the space-charge-limited current observed in diode mode. Fitting equations were developed based on experimental data to predict the dry cathode performance under a broader range of operational conditions. Calculations indicated that electron production cost could be less than 150 W/A, surpassing that of a water radio frequency (RF) cathode. The estimated emitter erosion rate was below , suggesting sufficient lifetime for HET operation. The thruster efficiency of a water-vapor HET employing the LaB dry cathode was estimated to reach 9.7% at a discharge voltage of 350 V and an anode mass flow rate of 0.68 mg/s, comparable to that of a xenon RF cathode. These results highlight the strong potential of LaB dry cathodes for use in water-vapor HETs.
期刊介绍:
Acta Astronautica is sponsored by the International Academy of Astronautics. Content is based on original contributions in all fields of basic, engineering, life and social space sciences and of space technology related to:
The peaceful scientific exploration of space,
Its exploitation for human welfare and progress,
Conception, design, development and operation of space-borne and Earth-based systems,
In addition to regular issues, the journal publishes selected proceedings of the annual International Astronautical Congress (IAC), transactions of the IAA and special issues on topics of current interest, such as microgravity, space station technology, geostationary orbits, and space economics. Other subject areas include satellite technology, space transportation and communications, space energy, power and propulsion, astrodynamics, extraterrestrial intelligence and Earth observations.