Author Details
Shevchenko, Yulia N.
Issue | Section | Title | File |
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) |