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...
| Main Authors: | , , |
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| Format: | Article |
| Language: | English |
| Published: |
Instituto de Aeronáutica e Espaço (IAE)
2021-11-01
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| Series: | Journal of Aerospace Technology and Management |
| Online Access: | https://www.jatm.com.br/jatm/article/view/1235 |