作者的详细信息
Василевский, Дмитрий Олегович
期 | 栏目 | 标题 | 文件 |
卷 23, 编号 4 (2022) | Section 2. Aviation and Space Technology | Increasing the specific impulse of an oxygen-hydrogen liquid rocket engine by increasing heat transfer in the combustion chamber |
(Rus) |
卷 22, 编号 1 (2021) | Section 2. Aviation and Space Technology | Development of the concept of a reusable liquid rocket engine with three-component fuel |
(Rus) (Eng) |
卷 22, 编号 2 (2021) | Section 2. Aviation and Space Technology | Design of the cooling system of a reasuble liquid rocket engine with three-component fuel |
(Rus) (Eng) |
卷 25, 编号 1 (2024) | Section 2. Aviation and Space Technology | Verification of thermodynamic parameters of a mixture of generator gas on oxygen-hydrogen fuel with an excess of one of the fuel components |
(Rus) (Eng) |