Ion–Electron Recombination and Heat Fluxes in High-Frequency Ion Thrusters
- 作者: Abgaryan V.K.1, Gidaspov V.Y.2, Nadiradze A.B.2, Semenov A.A.2
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隶属关系:
- Research Institute for Applied Mechanics and Electrodynamics, Moscow Aviation Institute (National Research University)
- Moscow Aviation Institute (National Research University)
- 期: 卷 45, 编号 2 (2019)
- 页面: 123-125
- 栏目: Article
- URL: https://bakhtiniada.ru/1063-7850/article/view/208210
- DOI: https://doi.org/10.1134/S1063785019020226
- ID: 208210
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详细
Heat fluxes emitted from plasma to the surface of structural elements of high-frequency (HF) ion thrusters with perforated electrodes of the ion-optical system have been studied. Radiation fluxes formed during ion–electron recombination on surfaces in contact with plasma are considered taking into account their spatial distribution and partial reflection from surfaces. New expressions for the heat fluxes are obtained that should be used as boundary conditions in numerical models for the calculation of temperature fields in HF ion thrusters.
作者简介
V. Abgaryan
Research Institute for Applied Mechanics and Electrodynamics, Moscow Aviation Institute (National Research University)
编辑信件的主要联系方式.
Email: vka.mai@mail.ru
俄罗斯联邦, Moscow, 125993
V. Gidaspov
Moscow Aviation Institute (National Research University)
Email: vka.mai@mail.ru
俄罗斯联邦, Moscow, 125993
A. Nadiradze
Moscow Aviation Institute (National Research University)
Email: vka.mai@mail.ru
俄罗斯联邦, Moscow, 125993
A. Semenov
Moscow Aviation Institute (National Research University)
Email: vka.mai@mail.ru
俄罗斯联邦, Moscow, 125993
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