Author Details

Шевченко, Юлия Николаевна

Issue	Section	Title	File
Vol 15, No 4 (2014)	Articles	Comparison of direct and reverse cycle of the thermal control system for the non-hermetic spacecrafts	(Rus)
Vol 24, No 1 (2023)	Section 2. Aviation and Space Technology	Design of a thermal control system with a two-phase coolant for a spacecraft with a capacity of 7 kW	(Rus)
Vol 21, No 3 (2020)	Section 2. Aviation and Space Technology	Flow dynamics in the radial-annular cavity of turbomachines	(Eng)
Vol 20, No 3 (2019)	Section 2. Aviation and Space Technology	Determining thermal resistance in the model of the liquid circuit of spacecraft thermal control system	(Eng)
Vol 20, No 3 (2019)	Section 2. Aviation and Space Technology	Calculation of complex heat transfer in the liquid circuit of the spacecraft thermal control system based on real topology and thermophysical properties	(Eng)
Vol 25, No 1 (2024)	Section 2. Aviation and Space Technology	Power engineering of the tangential supply device of the microturbine of the thermal control system of a promising spacecraft	(Rus) (Eng)