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Space-Rocket Complexes

Assessment of the efficiency of hot helium tank pressurization systems for oxygen-propelled rocket engines

¹Sukhyi KM, ²Voit SM, ¹Mitikov Yu.O, ²Spirkin SV, ¹Sukha IV. Assessment of the efficiency of hot helium tank pressurization systems for oxygen-propelled rocket engines. Space Science and Technology. 2025 ;31(4):03-11.

Analysis uf performance characteristics of aerospace systems

¹Kalynychenko DS, ²Manko TA. Analysis uf performance characteristics of aerospace systems. Space Science and Technology. 2024 ;30(6):15-19.

Features uf the march calculation supersonic flowing of a launch vehicle with a tori-shaped ring-wing

¹Timoshenko VI, ¹Galinskiy VP, ²Parshutkin AN. Features uf the march calculation supersonic flowing of a launch vehicle with a tori-shaped ring-wing. Space Science and Technology. 2024 ;30(6):03-14.

Evaluation of the scatter of liquid launch vehicle POGO oscillation amplitudes due to the influence of the scatter of internal factors

¹Pylypenko OV, ¹Dolgopolov SI, ¹Khoriak NV, ¹Nikolayev OD. 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.

Bifurcation state and rational design of three-layer reinforced compound cone-cylinder shell structure under combined loading

¹Grishchak VZ, ²Hryshchak DV, ³Dyachenko NM, ⁴Sanin AF, ⁵Sukhyy KM. Bifurcation state and rational design of three-layer reinforced compound cone-cylinder shell structure under combined loading. Space Science and Technology. 2023 ;29(6):026-041.

Conceptual design of the space industrial platform. Problem statement

¹Alpatov AP, ²Palii OS, ²Siutkina-Doronina SV. Conceptual design of the space industrial platform. Problem statement. Space Science and Technology. 2023 ;29(6):013-025.

Evaluation of the possibility of using polymers in the bodies of promising launch vehicles based on the heat resistance factor

¹Dreus AYu., ¹Dron ММ, ¹Dubovik LG, ¹Strembovskyi VV. Evaluation of the possibility of using polymers in the bodies of promising launch vehicles based on the heat resistance factor. Space Science and Technology. 2023 ;29(6):003-012.

On the possibility of launching spacecraft using light-class launch vehicle from the territory of Ukraine

¹Hladkyi EH, ¹Perlik VI, ¹Medvedev VV. On the possibility of launching spacecraft using light-class launch vehicle from the territory of Ukraine. Space Science and Technology. 2023 ;29(3):03-15.

Technical and economic substantiation of the air launch aerospace system parameters

¹Kalynychenko DS, ²Man'ko TA, ²Pavlenko VM, ³Pavlenko TYu. Technical and economic substantiation of the air launch aerospace system parameters. Space Science and Technology. 2023 ;29(2):03-09.

Mathematical modelling of start-up transients at clustered propulsion system with POGO-suppressors for CYCLON-4M launch vehicle

¹Pylypenko OV, ²Prokopchuk OO, ¹Dolgopolov SI, ¹Nikolayev OD, ¹Khoriak NV, ²Pysarenko VYu., ¹Bashliy ID, ²Polskykh SV. 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.

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