¹Nikolayev OD, ¹Bashliy ID, ²Rossi F, ³Marchan RA. High-frequency stability analysis of an aerospike rocket engine taking into account interaction of acoustics and vibrations of toroidal chamber structure. Space Science and Technology. 2026 ;32(1):13-26.

¹Sukhyi KM, ²Voit SM, ¹Mitikov Yu.O, ¹Sukha IV. The renaissance of the polytropic pressurization system for a rocket engine oxygen tank. Space Science and Technology. 2025 ;31(6):038-048.

¹Slusariev VV, ¹Busharskyi VL. Mathematical model of a liquid rocket engine cooling channel with local resistances. Space Science and Technology. 2025 ;31(5):03-10.

¹Tabatadze N, ¹Mazanishvili D, ¹Maisuradze A. Design and optimization of a propeller with increased energy efficiency. Space Science and Technology. 2025 ;31(4):22-30.

¹Boliubash Ye.S. Penetration of a cumulative jet of a pyrotechnic device into an obstacle of variable thicknes. Space Science and Technology. 2025 ;31(2):12-19.

Strelnikov НO, ¹Pryadko NS, ¹Ternova KV, ¹Katrenko МО. Choice if gas-dynamic thrust vector control typr in ricket engine project developments. Space Science and Technology. 2025 ;31(2):03-11.

¹Sokol GI, ²Kozin VS. Assessment of the possibility of introducing a solid propellant accelerator P230 of the Ariane 5 rocket as a Helmholtz resonator. Space Science and Technology. 2024 ;30(6):31-35.

¹Pryadko NS, ¹Strelnikov HO, ¹Ternova KV. The influence of the entrance angle to the bell-shaped tip of a shortened round supersonic nozzle of a rocket engine on its impulse characteristics. Space Science and Technology. 2024 ;30(3):53-60.

¹Minai OM, ¹Kuzmich IYu. 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.

¹Zhugan O, ¹Degtyarev MO. Version of loitering munitions classification based on the state-of-art and trends analysis. Space Science and Technology. 2024 ;30(3):31-39.