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Control on angles of attack and slip of the first stages of the launcher. Kosm. nauka tehnol. 2002 ;8(1):061-080.
. Controllability ensuring during stages separation of launch vechicle low controller effectiveness of second stage. Kosm. nauka tehnol. 2001 ;7(Supplement1):082-088.
. Creation of the Ukrainian meteor observation network: instruments, methods for processing, observatin possibilities. Space Science and Technology. 2022 ;28(4):39-70.
The cross-calibration method for “Sich-2” dat. Kosm. nauka tehnol. 2014 ;20(2):67-72.
. Definition of critical loading of loss of stability for three layer payload fairing with elastic longitudinal joints. Kosm. nauka tehnol. 2001 ;7(Supplement1):025-029.
. Degradation of parameters of solar cells under the influence of open space factors. Kosm. nauka tehnol. 2003 ;9(1):081-091.
. Deriving ultrapure three-dimensional semiconductor materials under space vacuum conditions. Kosm. nauka tehnol. 2003 ;9(5-6):030-032.
. The design of the power supply system for spacecraft of the microsatelute type. Kosm. nauka tehnol. 2003 ;9(Supplement1):101-105.
. Determination of a force transmitted by a plume of an ion thruster to an orbital object. Kosm. nauka tehnol. 2016 ;22(1):52-63.
. 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.
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