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Space-Rocket Complexes

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):04-04.

Conceptual design of the space industrial platform. Problem statement

¹Alpatov AP, ¹Palii OS, ¹Siutkina-Doronina SV. Conceptual design of the space industrial platform. Problem statement. Space Science and Technology. 2023 ;29(6):02-02.

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):01-01.

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.

Thermal strength of retention compartment interacting with exhaust gas

¹Degtyarev MA, ¹Akimov DV, ¹Bilous AS, ²Avramov KV. Thermal strength of retention compartment interacting with exhaust gas. Space Science and Technology. 2021 ;27(4):03-10.

Providing of POGO stability of the Cyclone-4M launch vehicle

¹Pylypenko OV, ²Degtyarev MA, ¹Nikolayev OD, ²Klimenko DV, ¹Dolgopolov SI, ¹Khoriak NV, ¹Bashliy ID, ²Silkin LA. Providing of POGO stability of the Cyclone-4M launch vehicle. Space Science and Technology. 2020 ;25(4):03-20.

Determination of the collective risk in a case of a launch vehicle «Cyclon-4M» crash during the flight phase using polygon images to represent populated areas

¹Gladkyi EG. Determination of the collective risk in a case of a launch vehicle «Cyclon-4M» crash during the flight phase using polygon images to represent populated areas. Space Science and Technology. 2020 ;26(3):32-41.

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