A. I. Morozov,1 V. M. Balebanov,2 A. I. Bugrova,3 A. S. Lipatov,3 V. K. Khartchevnikov3
1Kurchatov Institute Russian Research Ctr. (Russia) 2Institute of Cosmic Research (Russia) 3Moscow Institute of Radioengineering, Electronics, and Automation (Russia)
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The concept of a second generation Hall-current plasma accelerator (ATON-thruster), which has record performance characteristics is described. A method is proposed for analyzing the operation parameters of the accelerator on the basis of its performance characteristics. The results of measurements of plasma parameters in the accelerator channel and outflowing jet are presented. Influence of backmoving of particles from vacuum chamber to thruster one has been discussed.
A. I. Morozov,V. M. Balebanov,A. I. Bugrova,A. S. Lipatov, andV. K. Khartchevnikov
"ATON-thruster plasma accelerator", Proc. SPIE 4187, Fourth All-Russian Seminar on Problems of Theoretical and Applied Electron Optics, (2 August 2000); https://doi.org/10.1117/12.394146
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A. I. Morozov, V. M. Balebanov, A. I. Bugrova, A. S. Lipatov, V. K. Khartchevnikov, "ATON-thruster plasma accelerator," Proc. SPIE 4187, Fourth All-Russian Seminar on Problems of Theoretical and Applied Electron Optics, (2 August 2000); https://doi.org/10.1117/12.394146