Power loss to generating ion current in radio-frequency ion thrusters and technological sources of ions
- 作者: Abgaryan V.K.1, Riaby V.A.1, Yamashev G.G.2
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隶属关系:
- Research Institute of Applied Mechanics and Electrodynamics of Moscow Aviation Institute
- Moscow Aviation Institute
- 期: 卷 11, 编号 5 (2017)
- 页面: 1008-1013
- 栏目: Article
- URL: https://journals.rcsi.science/1027-4510/article/view/194177
- DOI: https://doi.org/10.1134/S1027451017050202
- ID: 194177
如何引用文章
详细
The balance of power in a radio-frequency ion source is constructed by calculating the inevitable power loss at surfaces bordering the inductive discharge plasma and power loss to the generation and preliminary acceleration of working-gas ions. The relationship between the specific radio-frequency power consumption per ion-current unit emerging from the source and electron temperature and geometric parameters of the gas discharge chamber is determined.
作者简介
V. Abgaryan
Research Institute of Applied Mechanics and Electrodynamics of Moscow Aviation Institute
编辑信件的主要联系方式.
Email: vka.mai@mail.ru
俄罗斯联邦, Moscow, 125080
V. Riaby
Research Institute of Applied Mechanics and Electrodynamics of Moscow Aviation Institute
Email: vka.mai@mail.ru
俄罗斯联邦, Moscow, 125080
G. Yamashev
Moscow Aviation Institute
Email: vka.mai@mail.ru
俄罗斯联邦, Moscow, 125993
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