作者的详细信息
Shilkin, Oleg V.
| 期 | 栏目 | 标题 | 文件 |
| 卷 24, 编号 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) |
| 卷 20, 编号 3 (2019) | Section 2. Aviation and Space Technology | Determining thermal resistance in the model of the liquid circuit of spacecraft thermal control system |
(Eng) |
| 卷 20, 编号 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) |