Informaçao sobre o Autor
Shilkin, Oleg V.
Edição | Seção | Título | Arquivo |
Volume 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) |
Volume 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) |
Volume 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) |