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Numerical simulation of a supersonic flow around finned boost vehicles. Space Science and Technology. 2017 ;23(5):33-43.
. Numerical simulation of efflux of a supersonic multicomponent chemical reacting rocket engine jet. Kosm. nauka tehnol. 2017 ;23(6):03-11.
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.
. Practical implementation of detection of spatiotemporal instability of atmosphere in the network of active reference stations UAEUPOS/ ZAKPOS. Kosm. nauka tehnol. 2017 ;23(1):54-62.
. Prospects of creating the reliable thermal barrier coating systems from elastomeric materials for solid propellant rocket engines. Kosm. nauka tehnol. 2017 ;23(6):46-50.
. Response of the authors to a review of the paper "Hybrid rocket engine on the methane clathrate" by A.S. Levenko, V.І. Prysiazhnyi, O.L. Pauk, A.S. Drozdenko. Kosm. nauka tehnol. 2017 ;23(1):15-17.
. Response of the authors to the commentary by G.V. Lizunov on our paper “Spatio-temporal dynamics of traveling ionospheric disturbances”. Space Science and Technology. 2017 ;23(2):52-67.
. The results of a complex research of functioning the GSS "SBIRS-Geo 2" in orbit. Kosm. nauka tehnol. 2017 ;23(1):63-70.
. Review of the paper "Hybrid rocket engine on the methane clathrate" by A.S. Levenko, V.І. Prysiazhnyi, O.L. Pauk, A.S. Drozdenko. Kosm. nauka tehnol. 2017 ;23(1):13-14.
The second approximation of the in-flight geometric calibration of a spacecraft imaging complex. Kosm. nauka tehnol. 2017 ;23(3):38-41.
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