Author Details
Vasilevsky, Dmitry O.
Issue | Section | Title | File |
Vol 23, No 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 |
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Vol 22, No 1 (2021) | Section 2. Aviation and Space Technology | Development of the concept of a reusable liquid rocket engine with three-component fuel |
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Vol 22, No 2 (2021) | Section 2. Aviation and Space Technology | Design of the cooling system of a reasuble liquid rocket engine with three-component fuel |
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Vol 25, No 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 |
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