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] Approximate models of plume flows from electric propulsion engines of spacecraft. Kosm. nauka tehnol. 1998 ;4(5):105–109.
Simulation of radiative electrization of spacecraft leeward surfaces in the ionosphere. Kosm. nauka tehnol. 2001 ;7(5-6):030-043.
Degradation of the electric power of solar arrays under the influence of the near-satellite environment in geostationary orbits. Kosm. nauka tehnol. 2002 ;8(4):025-036.
High-altitude spacecraft power losses of solar arrays as a result of interaction with environment. Kosm. nauka tehnol. 2004 ;10(4):039-049.
Degradation of polymeric materials for covering spacecraft solar arrays under exposure to atomic oxygen flows. Kosm. nauka tehnol. 2005 ;11(5-6):078-086.
Fast-electron charge transfer at downwind surfaces of spacecrafts in the Earth's polar ionosphere. Kosm. nauka tehnol. 2007 ;13(6):005-017.
Molecular contamination of spacecraft surfaces in thermostatic control and orbital injection of launch vehicle nose cone. Kosm. nauka tehnol. 2007 ;13(3):003-011.
Effects of magnetohydrodynamic control in heat exchange and decelaration of magnetized bodies in the earth's atmosphere and magnetosphere. Kosm. nauka tehnol. 2008 ;14(4):27-38.
Magnetohydrodynamic deceleration of «magnetized» planets in solar wind plasma. Kosm. nauka tehnol. 2009 ;15(6):03-13.
Power losses for solar arrays of a spacecraft in the Earth’s polar ionosphere and magnetosphere. Kosm. nauka tehnol. 2011 ;17(3):05-15.