1. Approximate determination of losses in characteristic velocity and increments in flight altitude of the multistage launch vehicle upper stages;Proceedings of Higher Educational Institutions. Маchine Building;2023-08
2. Selection of the optimal thrust-to-weight ratio of the first stages of small-lift launch vehicles;Proceedings of Higher Educational Institutions. Маchine Building;2023-06
3. Study of the dependence of an air jet shape on pressure in a Laval nozzle;VII INTERNATIONAL CONFERENCE “SAFETY PROBLEMS OF CIVIL ENGINEERING CRITICAL INFRASTRUCTURES” (SPCECI2021);2023
4. An approximate determination of the characteristic velocity losses of the last stages of launch vehicles;XLV ACADEMIC SPACE CONFERENCE, DEDICATED TO THE MEMORY OF ACADEMICIAN S.P. KOROLEV AND OTHER OUTSTANDING NATIONAL SCIENTISTS — PIONEERS OF SPACE EXPLORATION;2023
5. An approximate determination of the characteristic velocity losses and the flight altitude increment of the second stages of three-stage launch vehicles;XLV ACADEMIC SPACE CONFERENCE, DEDICATED TO THE MEMORY OF ACADEMICIAN S.P. KOROLEV AND OTHER OUTSTANDING NATIONAL SCIENTISTS — PIONEERS OF SPACE EXPLORATION;2023