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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.
. Determination of the optimum design of the means to ensure the fuel continuity by the method of numerical simulation. Космічна наука і технологія. 2024 ;30(3):40-52.
Determination of the orientation of the artificial Earth satellite in the case of diffusive scattering of light by its surface. Space Science and Technology. 2022 ;28(1):61-69.
. Determination of the regional elipsoid for Ukraine and its efficiency. Space Science and Technology. 2024 ;30(5):09-09.
. Determination of the temperature mode, duration of presence of the human adenovirus on orbital space stations and influence of clinorotation on some properties of the virus. Kosm. nauka tehnol. 2003 ;9(1):096-101.
Determining of limit possible deviations of sandwich panels honeycomb core manufacturing. Kosm. nauka tehnol. 2004 ;10(Supplement1):083-086.
. Determining spacecraft orientation using information from two jointly processed star trackers. Kosm. nauka tehnol. 2014 ;20(3):22-27.
. Development and investigation of solar batteries for the solar energy system of the UKRAINIAN YOUTH SATELLITE. Kosm. nauka tehnol. 2005 ;11(3-4):092-095.
. Development and investigation of transformable-volume structures for space applications. Kosm. nauka tehnol. 2015 ;21(4):32–38.
. Development of a high-speed software package for calculating the trajectory of launching a spacecraft into a geostationary orbit using the gravitational field of the moon with visualization of calculations. Kosm. nauka tehnol. 2004 ;10(Supplement1):059-062.
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