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):04-04.

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.

¹Abada O, ¹Kbab H, ¹Haif S. Optimizing the design of a supersonic Planar Dual Bell Nozzle (PDBN). Space Science and Technology. 2024 ;30(2):15-27.

¹Minai OM. Classification, main types of structures and purpose of capilary means to ensure fuel perfection. Space Science and Technology. 2024 ;30(1):14-30.

¹Pryadko NS, ¹Strelnikov HO, ¹Ternova KV. Research of supersonic flow in shortened nozzles of rocket engines with a bell-shaped tip. Space Science and Technology. 2024 ;30(1):03-13.

¹Pecheritsa LL, ¹Smіla ТG. Application of the test-particle statistical method for the simulation of rarefied plume in a vacuum. Space Science and Technology. 2023 ;29(4):012-023.

¹Golubek AV, ²Dron' MM, ³Petrenko OM. Estimation of the possibility of using electric propulsion system for large-sized orbital debris postmission disposal. Space Science and Technology. 2023 ;29(3):34-46.

¹Redka MO, ²Khoroshylov SV. Determination of the force impact of an ion thruster plume on an orbital object via deep learning. Space Science and Technology. 2022 ;28(5):15-26.