The possibility of determining the rate of erosion of the discharge chamber of a thruster with closed electron drift and extended zone of acceleration using the method of emission spectroscopy

Author:

Gorshkov O. A.,Dyshlyuk E. N.,Shagaida A. A.

Publisher

Pleiades Publishing Ltd

Subject

General Engineering,Condensed Matter Physics

Reference19 articles.

1. Gorshkov, O. and Koroteev, A., New Trends in Hall Effect Thruster Development, in Proc. Propulsion for Space Transportation of the XXI Century Conf., Versailles, 2002.

2. Sputtering by Particle Bombardment III, Behrisch, R.. and Wittmaack, K., Eds., Berlin: Heidelberg, 1991.

3. Semenov, A.A. and Shkarban, I.I., RKT: Raketnye Dvigateli i Energeticheskie Ustanovki, 1991, no. 3, p. 42.

4. Khartov, S.A., Egorov, V.K., Nadiradze, A.B., and Zikeeva, Yu.V., Angular Distribution of Ceramic Isolator Sputtered Material in the SPT Jet, in Proc. 30th Int. Electric Propulsion Conf. IEPC-2003-052, Toulouse, 2003.

5. Garnier, Y., Viel, V., Roussel, J.F. et al., Investigation of Xenon Ion Sputtering of One Ceramic Material Used in SPT Discharge Chamber, in Proc. 27th Int. Electric Propulsion Conf. IEPC-1999-083, Kitakyushu, 1999, p. 512.

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