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Degradation of polymeric materials for covering spacecraft solar arrays under exposure to atomic oxygen flows. Kosm. nauka tehnol. 2005 ;11(5-6):078-086.
. High-altitude spacecraft power losses of solar arrays as a result of interaction with environment. Kosm. nauka tehnol. 2004 ;10(4):039-049.
. Dynamic effect of a plasma beam on a space debris object. Kosm. nauka tehnol. 2017 ;23(1):36-49.
. Simulation of radiative electrization of spacecraft leeward surfaces in the ionosphere. Kosm. nauka tehnol. 2001 ;7(5-6):030-043.
. The plume-flows structure of spacecraft thrusters. Kosm. nauka tehnol. 2003 ;9(4):017-025.
. 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.
. Power losses for solar arrays of a spacecraft in the Earth’s polar ionosphere and magnetosphere. Kosm. nauka tehnol. 2011 ;17(3):05-15.
. Acceleration of resource tests of spacecraft polymers for resistance to long-term influence of atomic oxygen in the Earth ionosphere. Space Science and Technology. 2021 ;27(4):54-64.
. Contact diagnostics of the ionosphere and laboratory plasma. Kosm. nauka tehnol. 2004 ;10(2-3):003-015.
. Fast-electron charge transfer at downwind surfaces of spacecrafts in the Earth's polar ionosphere. Kosm. nauka tehnol. 2007 ;13(6):005-017.
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