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[1] M. B. Belikov, O. A. Gorshkov, “High-performance low power Hall thruster”, AIAA-2001-3780, AIAA Joint Propulsion Conference and Exhibit, 37th (Salt Lake City, UT, July 8-11), 2001
[2] J. J. Szabo, Fully Kinetic Numerical Modeling of a Plasma Thruster, Ph.D. Thesis, MIT, 2001
[3] G. Bërd, Molekulyarnaya gazovaya dinamika, Izd. Mir, M., 1980
[4] Ch. Bedsel, A. Lengdon, Fizika plazmy i chislennoe modelirovanie, EnergoAtomIzdat, M., 1989
[5] R. Khokni, Dzh. Istvud, Chislennoe modelirovanie metodom chastits, Mir, M., 1987
[6] S. V. Irishkov,O. A. Gorshkov, A. A. Shagayda, Fully Kinetic Modeling of Low-Power Hall Thrusters, IEPC-2005-035 (October 31 – November 4), Princeton, New Jersey, USA, 2005
[7] N. V. Blinov, O. A. Gorshkov, R. N. Rizakhanov, A. A. Shagayda, Hall-Effect Thruster with High Specific Impulse, Proc. 4th International Spacecraft Propulsion Conf. (Sardinia, Italy, 2–9 June 2004)
[8] V. Blateau, M. Martinez-Sanchez, O. Batishchev, J. Szabo, “PIC Simulation of High Specific Impulse Hall Effect Thruster”, IEPC-01-037, 27th International Electric Propulsion Conference (Pasadena, CA, 15–19 October), 2001
[9] Noah Warner, James Szabo, Manuel Martinez-Sanchez, “Characterization of a high specific impulse Hall Thruster Using Electrostatic Probes”, IEPC-2003-082, 28th International Electric Propulsion Conference, Toulouse, France, 2003
[10] N. V. Blinov, O. A. Gorshkov, A. A. Shagayda, “Experimental Investigation of Magnetic Field Topology Influence on Structure of Accelerating Layer and Performance of Hall Thruster”, IEPC-2005-033, 29th International Electric Propulsion Conference, Princeton, 2005