Computational and Experimental Study on the Discharge Model of a 20 Amperes Emission Current Hollow Cathode
The discharge characteristics of hollow cathode directly affect the performance of thruster. In order to obtain the plasma parameters of the 20 A emission current hollow cathode, COMSOL software is used to simulate the potential distribution, neutral fluid distribution and plasma parameters of the c...
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| Autores principales: | , , |
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| Formato: | article |
| Lenguaje: | EN |
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Departamento de Ciência e Tecnologia Aeroespacial
2021
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| Materias: | |
| Acceso en línea: | https://doi.org/10.1590/jatm.v13.1235 https://doaj.org/article/4d224f49005a4c6c9561077b56bd1c86 |
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