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] Evaluation of the scatter of liquid launch vehicle POGO oscillation amplitudes due to the influence of the scatter of internal factors. Space Science and Technology. 2024 ;30(3):01-01.
Development of vibration protection systems of spacecraft – state of the art and perspectives. Space Science and Technology. 2023 ;29(5):003-019.
The approach to numerical simulation of the spatial movement of fluid with forming free gas inclusions in propellant tank at space flight conditions. Space Science and Technology. 2022 ;28(5):03-14.
Mathematical modelling of start-up transients at clustered propulsion system with POGO-suppressors for CYCLON-4M launch vehicle. Space Science and Technology. 2021 ;27(6):003-015.
Mathematical modeling of dynamic processes in feeding system of space stage main engine of launch vehicle at active and passive flight. Space Science and Technology. 2020 ;26(1):03-17.
Providing of POGO stability of the Cyclone-4M launch vehicle. Space Science and Technology. 2020 ;25(4):03-20.
Pequliarities of mathematical modeling of low-frequency dynamics of the staged liquid rocket sustainer engines at its startup. Space Science and Technology. 2017 ;23(5):03-13.
About the classification of launch equipment of the space launch systems for the strength standards justification. Kosm. nauka tehnol. 2016 ;22(1):03-14.
Scientific, technical and methodic support of space and rocket technology development and operation. Kosm. nauka tehnol. 2014 ;20(6):35-48.
Development of research and educational program for involving Ukraine's young people in space research. Kosm. nauka tehnol. 2006 ;12(4):104-108.