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Design aspects of ensuring of a launch vehicle operation. Kosm. nauka tehnol. 2016 ;22(2):03-11.
. Determination of a force transmitted by a plume of an ion thruster to an orbital object. Kosm. nauka tehnol. 2016 ;22(1):52-63.
. Dynamic impact interaction of space constructions adapters during separation. Kosm. nauka tehnol. 2016 ;22(2):12-21.
. Degradation of spacecraftpolymer films on long exposure to atomic oxygen flows and vacuum ultraviolet radiation. Kosm. nauka tehnol. 2015 ;21(5):57–68.
. Determination of orientation, coordinates, relative position and movement parameters of objects in space with the GNSS technology. Kosm. nauka tehnol. 2015 ;21(2):40–46.
. Determination of the hazardous zones in the impact areas of separated parts of launch vehicles under the uncertain altitude of their initial destruction. Kosm. nauka tehnol. 2015 ;21(6):49–55.
. Development and investigation of transformable-volume structures for space applications. Kosm. nauka tehnol. 2015 ;21(4):32–38.
. The development of modern means of spacecraft integration with a launch vehicle. Kosm. nauka tehnol. 2015 ;21(5):18–23.
. Development of robust methods of precision attitude control of small spacecrafts and their implementation at the problem-oriented processors. Kosm. nauka tehnol. 2015 ;21(1):03–09.
. The development of the imaging polarimeter’s polarizer on the basis of the polarizing film. Kosm. nauka tehnol. 2015 ;21(4):19–23.
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