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Space Energy, Power and Propulsion

Estimation of the possibility of using electric propulsion system for large-sized orbital debris postmission disposal

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):03-03.

Determination of the force impact of an ion thruster plume on an orbital object via deep learning

¹Redka MO, ¹Khoroshylov 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.

The approach to numerical simulation of the spatial movement of fluid with forming free gas inclusions in propellant tank at space flight conditions

¹Pylypenko OV, ²Smolenskyy DE, ¹Nikolayev OD, ¹Bashliy ID. The approach to numerical simulation of the spatial movement of fluid with forming free gas inclusions in propellant tank at space flight conditions. Space Science and Technology. 2022 ;28(5):03-14.

Approach to solution of tank with hydrogen peroxide pressurization by its decomposition products

¹Andriievskyi MV, ²Mitikov Yu.O. Approach to solution of tank with hydrogen peroxide pressurization by its decomposition products. Space Science and Technology. 2021 ;27(5):003-010.

Tte stage deorbiting with a deceleration pulse detonation engine

¹Zolotko OE, ¹Zolotko OV, ¹Sosnovska OV, ¹Aksyonov OS, ¹Savchenko IS. Tte stage deorbiting with a deceleration pulse detonation engine. Space Science and Technology. 2021 ;27(4):32-41.

Influence of propellant leakage from pump area into turbine area on turbo-pump operation stability

¹Andriievskyi MV, ²Mitikov Yu.O. Influence of propellant leakage from pump area into turbine area on turbo-pump operation stability. Space Science and Technology. 2021 ;27(1):97-102.

The influence of gas-dynamic processes on acoustic radiation in the interaction of impinging jet with the flat plate

¹Nikolin SO, ¹Sokol GI. The influence of gas-dynamic processes on acoustic radiation in the interaction of impinging jet with the flat plate. Space Science and Technology. 2020 ;26(3):20-31.

Study of the temperature and force effects of supersonic jets of the space rockets on the gas duct of the launch complex during the water supply system operation

¹Mochonov RA, ¹Sotnichenko AV, ¹Ivanytskyi HM, ¹Salo MP. Study of the temperature and force effects of supersonic jets of the space rockets on the gas duct of the launch complex during the water supply system operation. Space Science and Technology. 2020 ;26(3):03-19.

Mathematical modeling of the processes of air gas thermodynamics of the supersonic aircraft with a ramjet

¹Timoshenko VI, ¹Galinskiy VP. Mathematical modeling of the processes of air gas thermodynamics of the supersonic aircraft with a ramjet. Space Science and Technology. 2020 ;26(2):03-18.

Problems and ways of their solutions in the development of a lowthrust liquid jet engine for a stage 3 liquid jet system of «Cyclone-4» launch vehicle

¹Durachenko VM, ¹Shpak AV, ¹Kolesnychenko SA, ¹Aheyeva LI, ¹Dolinkevich AS, ¹Unchur KO. Problems and ways of their solutions in the development of a lowthrust liquid jet engine for a stage 3 liquid jet system of «Cyclone-4» launch vehicle. Space Science and Technology. 2020 ;26(1):18-29.

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