Отправить статью по E-mail Power loss to generating ion current in radio-frequency ion thrusters and technological sources of ions
- Авторы: Abgaryan V.K.1, Riaby V.A.1, Yamashev G.G.2
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Учреждения:
- Research Institute of Applied Mechanics and Electrodynamics of Moscow Aviation Institute
- Moscow Aviation Institute
- Выпуск: Том 11, № 5 (2017)
- Страницы: 1008-1013
- Раздел: Article
- URL: https://journals.rcsi.science/1027-4510/article/view/194177
- DOI: https://doi.org/10.1134/S1027451017050202
- ID: 194177
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Аннотация
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.
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V. Abgaryan
Research Institute of Applied Mechanics and Electrodynamics of Moscow Aviation Institute
Автор, ответственный за переписку.
Email: vka.mai@mail.ru
Россия, Moscow, 125080
V. Riaby
Research Institute of Applied Mechanics and Electrodynamics of Moscow Aviation Institute
Email: vka.mai@mail.ru
Россия, Moscow, 125080
G. Yamashev
Moscow Aviation Institute
Email: vka.mai@mail.ru
Россия, Moscow, 125993
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