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Space Energy, Power and Propulsion

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.

Mathematical modeling of dynamic processes in feeding system of space stage main engine of launch vehicle at active and passive flight

¹Pylypenko OV, ¹Nikolayev OD, ²Bashliy ІD, ¹Dolgopolov SI. Mathematical modeling of dynamic processes in feeding system of space stage main engine of launch vehicle at active and passive flight. Space Science and Technology. 2020 ;26(1):03-17.

Estimation of fuel consumption for maintenance of average height of a space vehicle

¹Bakhtinov OM, ²Avdeev VV. Estimation of fuel consumption for maintenance of average height of a space vehicle. Kosm. nauka tehnol. 2004 ;10(Supplement1):063-064.

Ensuring re-launch in flight of the steering engine, made according to the scheme with afterburning of generator gas

¹Prokopenko Yu.A, ¹Strelchenko EV, ¹Pisarenko VYu., ¹Sinitsyn DYu., ¹Troyak AB, ¹Shementov AN. Ensuring re-launch in flight of the steering engine, made according to the scheme with afterburning of generator gas. Kosm. nauka tehnol. 2004 ;10(Supplement1):034-038.

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