Polyatomic Ion-Induced Electron Emission (IIEE) in Electrospray Thrusters
To better characterize the lifetime and performance of electrospray thrusters, electron emission due to electrode impingement by the propellant cation 1-ethyl-3-methylimidazolium (EMI<sup>+</sup>) has been evaluated with semi-empirical modeling techniques. Results demonstrate that electron emission...
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| Autors principals: | , , |
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| Format: | Artigo |
| Idioma: | Inglês |
| Publicat: |
MDPI AG
2020-10-01
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| Col·lecció: | Aerospace |
| Matèries: | |
| Accés en línia: | https://www.mdpi.com/2226-4310/7/11/153 |
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