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Information × Registration Number 0219U102210, 0119U102577 , R & D reports Title Development of structural chart and research of auxiliary control system of launch vehicle stage with the use of detonation engine popup.stage_title Head Ternova Kateryna V., Кандидат технічних наук Registration Date 21-12-2019 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 study is an auxiliary rocket space control system in full-time and freelance conditions on the active rocket flight section. The purpose of scientific research at this stage is to develop schematic solutions for the implementation of a new auxiliary rocket space control system in emergency situations. Research methods include numerical and experimental ones. The following are the results obtained at this stage of work: - Possibilities to increase mass-energy characteristics of engine installations of upper stages of launch vehicles are considered; - a structural diagram of an auxiliary rocket space control system using a detonation engine was developed; - the experimental base of ITM NASU and SSAU was prepared for the study of gas-dynamic processes in the developed auxiliary system of upper rocket carrier control and the program of experimental researches of the scheme of the auxiliary system for upper rocket carrier control at the stage of its operation was developed. The results of the research will allow the development of a new auxiliary system to control the rocket space stage using a detonation engine to blow gas into the closed part of the nozzle, which will significantly improve the reliability of flight stabilization. Developed design scheme, the procedure for theoretical and experimental research is intended to be used to improve the existing systems of space rocket control. The results of the work can be used in the creation of auxiliary systems of space rocket control in emergency situations, as well as the basis for other studies of propulsion systems with a controlled thrust vector. Product Description popup.authors Yevseienko Maksym V. Vasyliv Stepan S. popup.nrat_date 2020-04-02 Close