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Information × Registration Number 0223U004995, 0123U103085 , R & D reports Title Development of a methodology for assessing the impact of high-energy systems on supersonic flow popup.stage_title Head Vasyliv Stepan S., Кандидат технічних наук Registration Date 12-12-2023 Organization Institute of Technical Mechanics of the National Academy of Sciences of Ukraine and the State Space Agency of Ukraine popup.description2  The object of the study is gas-dynamic control of the direction of the rocket thrust vector. The goal of scientific research at this stage is the development of schematic solutions for the detonation process application to control the flight of the rocket. Development of assessing methods for the impact of detonation products and shock waves on an anti-aircraft missile in flight. Preparation of an experimental base for conducting research. Research methods – computational and experimental methods of analyzing the impact of detonation products and shock waves on the supersonic flow. Below there are the results obtained at this stage of work: – methods of gas-dynamic control of an anti-aircraft missile were analyzed and schematic solutions for the missile flight control used the corded detonation engine were developed; – methods of the impact assessing detonation products and shock waves on the generated control forces and the missile body in flight were developed; - preparation of a test bench for research was carried out. The results of the research make it possible to develop a methodology for improving the control systems of anti-aircraft missiles, as well as fast-acting gas-dynamic anti-aircraft missile controls. The obtained research results allow a deeper study of the processes in the gas-dynamic system of anti-aircraft missile control, which is especially relevant for increasing the defense capability of Ukraine. Product Description popup.authors Ternova Kateryna V. popup.nrat_date 2023-12-12 Close