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Information × Registration Number 0214U008383, 0114U003484 , R & D reports Title Study of features and mechanisms for the control of spacecraft orbital motion in a conducting medium. Stage 2 - "Dynamics of interaction between magnetized spacecraft and electrodynamic cable system with conductive media" popup.stage_title Head Shuvalov Valentyn Oleksievych; Alpatov Anatoliy Petrovych, Registration Date 23-12-2014 Organization The Institute of Technical Mechanics of the National Academy of Sciences of Ukraine and the State Space Agency of Ukraine popup.description2 Object of research - direction 1: "magnetized" sphere in a hypersonic flow of rarefied plasma under conditions of simulation of the interaction between a spacecraft and the ionospheric plasma and the solar wind plasma; direction 2: dynamics of electrodynamic space tethered system. Method of research - experimental, methods of theoretical mechanics and space flight mechanics, ionized plasma physics, mathematical modeling, numerical solution of ordinary differential equations and computer visualization. Obtained results. Direction 1: The possibility and effectiveness of the dynamic interaction control by means of own magnetic field rotation around the velocity vector of the hypersonic flow of the rarefied plasma have been scientifically proved; features of interaction "spacecraft - plasma" were studied under conditions of spacecraft moving in the Earth's ionosphere at altitudes from 800 to 1000 km and in the interplanetary space; the structure of the perturbation zone near the "magnetized" body has been investigated experimentally, dependences of "magnetic" constituents of the drag and lift force coefficients of "magnetized" sphere in the hypersonic flow of rarefied plasma vs. the angle between the velocity vector and the induction vector of the body’s magnetic field within the wide range of the body’s magnetic field pressure and gasdynamic plasma flow pressure. Direction 2. Revised and developed mathematical and computer models of the dynamics of electrodynamic space tethered system and to study the basic laws of dynamics of the system, including: the regularities of deployment depending on the parameters of a flexible connection and speed of deployment; the regularities of resonance in the dynamics of the radial tether system to reflect changes in the plasma density at the motion of the system in the Earth's ionosphere; the simple model and estimates of the rate of withdrawal for the 10 kilometer space tethered system; studied small aerodynamic resonant oscillations of the radial system. Scope of application - direction 1: Mechanics of fluid, gas and plasma. Scientific researches in this field are relevant for space-developed countries. The results can be used in the preparation of onboard scientific experiments as well as the development of future space crafts with magneto hydrodynamic (MHD) motion control systems; direction 2: space exploration, space systems dynamics. The results can be used to study the laws of nonlinear motion of electrodynamic space tethered system and to choice of parameters for the experimental system. Product Description popup.authors Алпатов А.П. Кочубей Г.С. Кулагін С.М. Лазученков Д.М. Маслова А.І. Носіков С.В. Пироженко О.В. Письменний М.І. Пурцеладзе А.А. Різниченко М.П. Токмак М.А. Федякина Н.М. Храмов Д.О. Шувалов В.О. Шупілова Л.М. popup.nrat_date 2020-04-02 Close