Power loss to generating ion current in radio-frequency ion thrusters and technological sources of ions
- Авторлар: Abgaryan V.K.1, Riaby V.A.1, Yamashev G.G.2
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Мекемелер:
- Research Institute of Applied Mechanics and Electrodynamics of Moscow Aviation Institute
- Moscow Aviation Institute
- Шығарылым: Том 11, № 5 (2017)
- Беттер: 1008-1013
- Бөлім: Article
- URL: https://journals.rcsi.science/1027-4510/article/view/194177
- DOI: https://doi.org/10.1134/S1027451017050202
- ID: 194177
Дәйексөз келтіру
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.
Негізгі сөздер
Авторлар туралы
V. Abgaryan
Research Institute of Applied Mechanics and Electrodynamics of Moscow Aviation Institute
Хат алмасуға жауапты Автор.
Email: vka.mai@mail.ru
Ресей, Moscow, 125080
V. Riaby
Research Institute of Applied Mechanics and Electrodynamics of Moscow Aviation Institute
Email: vka.mai@mail.ru
Ресей, Moscow, 125080
G. Yamashev
Moscow Aviation Institute
Email: vka.mai@mail.ru
Ресей, Moscow, 125993
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