Power loss to generating ion current in radio-frequency ion thrusters and technological sources of ions


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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

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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