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This article is cited in 5 scientific papers (total in 5 papers)
Ion–electron recombination and heat fluxes in high-frequency ion thrusters
V. K. Abgaryana, V. Yu. Gidaspovb, A. B. Nadiradzeb, A. A. Semenovb a State Research Institute of Apply Mechanics and Electrodynamics of MAI
b Moscow Aviation Institute (National Research University)
Abstract:
Heat fluxes emitted from plasma to the surface of structural elements of high-frequency (HF) ion thrusters with perforated electrodes of the ion-optical system have been studied. Radiation fluxes formed during ion–electron recombination on surfaces in contact with plasma are considered taking into account their spatial distribution and partial reflection from surfaces. New expressions for the heat fluxes are obtained that should be used as boundary conditions in numerical models for the calculation of temperature fields in HF ion thrusters.
Received: 30.10.2018 Revised: 30.10.2018 Accepted: 15.11.2018
Citation:
V. K. Abgaryan, V. Yu. Gidaspov, A. B. Nadiradze, A. A. Semenov, “Ion–electron recombination and heat fluxes in high-frequency ion thrusters”, Pisma v Zhurnal Tekhnicheskoi Fiziki, 45:4 (2019), 3–5; Tech. Phys. Lett., 45:2 (2019), 123–125
Linking options:
https://www.mathnet.ru/eng/pjtf5522 https://www.mathnet.ru/eng/pjtf/v45/i4/p3
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