On the Cost of Ion Production in Radio-Frequency Ion Thrusters and Technological Ion Sources


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Abstract

The power balance in the inductive discharge of a radio-frequency ion source is worked out by calculating the power losses caused by plasma deposition on the surfaces bordering it, by the power consumed for positive-ion generation and pre-acceleration, by eddy currents, and by propellant-atom excitation. The relationship between the minimal consumption of high-frequency power per unit of ion current of the thruster and electron temperature and geometric parameters of the gas-discharge chamber is presented.

About the authors

V. K. Abgaryan

Research Institute of Applied Mechanics and Electrodynamics of Moscow Aviation Institute (National Research University)

Author for correspondence.
Email: vka.mai@mail.ru
Russian Federation, Moscow, 125080

K. I. Kruglov

Research Institute of Applied Mechanics and Electrodynamics of Moscow Aviation Institute (National Research University)

Email: vka.mai@mail.ru
Russian Federation, Moscow, 125080

A. I. Mogulkin

Research Institute of Applied Mechanics and Electrodynamics of Moscow Aviation Institute (National Research University)

Email: vka.mai@mail.ru
Russian Federation, Moscow, 125080

V. A. Obukhov

Research Institute of Applied Mechanics and Electrodynamics of Moscow Aviation Institute (National Research University)

Email: vka.mai@mail.ru
Russian Federation, Moscow, 125080

V. A. Riaby

Research Institute of Applied Mechanics and Electrodynamics of Moscow Aviation Institute (National Research University)

Email: vka.mai@mail.ru
Russian Federation, Moscow, 125080

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