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] 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 regional elipsoid for Ukraine and its efficiency. Space Science and Technology. 2024 ;30(5):87-95.
. Dtnamic model of vector motion and its application in spacecraft unaxial orientation problems. Space Science and Technology. 2024 ;30(4):24-33.
. Electron-beam gun for manual electron-beam welding in lunar surface conditions. Space Science and Technology. 2024 ;30(1):80-91.
. Elements of technology of electron-beam welding of aluminium alloys for installation and repair-restoration work on the surface of the Moon. Space Science and Technology. 2024 ;30(2):40-53.
. 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):03-15.
. Features uf the march calculation supersonic flowing of a launch vehicle with a tori-shaped ring-wing. Space Science and Technology. 2024 ;30(6):01-01.
. Feed-forwardcontrol of additional deployment of a space tether with recovery of its initial vertical orientation. Space Science and Technology. 2024 ;30(5):03-18.
Geospatial analysis of the potential of the territories of Ukraine for the placement of solar power plants based on satellite data. Space Science and Technology. 2024 ;30(1):31-43.
In memory of Prof. Elizabeth KORDYUM. Space Science and Technology. 2024 ;30(3):95-96.