Analysis uf performance characteristics of aerospace systems 1Kalynychenko DS, 2Man'ko TA. Analysis uf performance characteristics of aerospace systems. Space Science and Technology. 2024 ;30(6):02-02.
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):01-01.
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.
Performance of interface hoses for thermal conditioning system of "Cyclon-4" space rocket in extreme conditions 1Khorolskyi MS, Bigun SO. Performance of interface hoses for thermal conditioning system of "Cyclon-4" space rocket in extreme conditions. Space Science and Technology. 2021 ;27(4):11-20.