Power loss to generating ion current in radio-frequency ion thrusters and technological sources of ions
- Authors: Abgaryan V.K.1, Riaby V.A.1, Yamashev G.G.2
-
Affiliations:
- Research Institute of Applied Mechanics and Electrodynamics of Moscow Aviation Institute
- Moscow Aviation Institute
- Issue: Vol 11, No 5 (2017)
- Pages: 1008-1013
- Section: Article
- URL: https://journal-vniispk.ru/1027-4510/article/view/194177
- DOI: https://doi.org/10.1134/S1027451017050202
- ID: 194177
Cite item
Abstract
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.
About the authors
V. K. Abgaryan
Research Institute of Applied Mechanics and Electrodynamics of Moscow Aviation Institute
Author for correspondence.
Email: vka.mai@mail.ru
Russian Federation, Moscow, 125080
V. A. Riaby
Research Institute of Applied Mechanics and Electrodynamics of Moscow Aviation Institute
Email: vka.mai@mail.ru
Russian Federation, Moscow, 125080
G. G. Yamashev
Moscow Aviation Institute
Email: vka.mai@mail.ru
Russian Federation, Moscow, 125993
Supplementary files
