Персона: Терехов, Святослав Алексеевич
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Acceleration of Dusty Plasma Flow in Azimuthal Electric and Radial Magnetic Fields
2020, Karimov, A. R., Terekhov, S. A., Shikanov, A. E., Каримов, Александр Рашатович, Терехов, Святослав Алексеевич, Шиканов, Александр Евгеньевич
© 2020, Pleiades Publishing, Ltd.Abstract: In the framework of the model of cold hydrodynamics, acceleration of the flow of dusty plasma in azimuthal electric and radial magnetic fields has been studied. The obtained results show that there are conditions under which macroscopic particles are captured and accelerated by the plasma flow.
Use of Plasma Flows to Clean the Near-Earth Space
2021, Yamshchikov, V. A., Karimov, A. R., Terekhov, S. A., Shikanov, A. E., Каримов, Александр Рашатович, Терехов, Святослав Алексеевич, Шиканов, Александр Евгеньевич
© 2021, Pleiades Publishing, Ltd.Abstract: A system for cleaning near-Earth space from space debris in the upper layers of the atmosphere is proposed, which is based on a plasma accelerator that uses the medium of the upper layers of the atmosphere and solar radiation to generate plasma flows of the required intensity. Estimates of the main material and energy characteristics of the system were obtained, which demonstrate the feasibility of the proposed device.
Electrophysical Means in Space Research and Applications for the near-Earth Space
2021, Murad, P. A., Yamschikov, V., Karimov, A. R., Terekhov, S. A., Каримов, Александр Рашатович, Терехов, Святослав Алексеевич
© 2021, American Institute of Aeronautics and Astronautics Inc.. All rights reserved.The paper discusses the use of the interplanetary substance as a possible fuel for spacecraft’s plasma thrusters for interplanetary flights and the possibility of creation the electrodynamic space debris collection system in the upper atmosphere based on a plasma propulsor using the upper atmosphere medium and solar radiation to create plasma flows of the required intensity. The intensity is such that the debris is used for propellant as well as storage of the space debris. Moreover, the device would use a magnetic field to convert linear momentum of the debris into angular momentum for capture. Estimates of the basic material and energy characteristics of this state-of-the art system are obtained, which demonstrate the technical feasibility of the proposed device. Furthermore, the accelerator may also use plasma with motion of some of the debris as propellant.