Zobrazeno 1 - 10
of 20
pro vyhledávání: '"V S Zakharchenko"'
Autor:
A. R. Polyakov, O. A. Smolyakov, E. A. Ozdoeva, A. M. Neklyudova, V. S. Zakharchenko, А. N. Varyukhin
Publikováno v:
Вестник университета, Vol 0, Iss 3, Pp 117-126 (2023)
In order to develop a methodological apparatus for assessing various stages of the life cycle of hybrid/electric propulsion units, the existing approaches to estimating the costs of developing, manufacturing and operating aircraft engines of the trad
Externí odkaz:
https://doaj.org/article/8905c5e6520644f8ba7d8ad866560146
Autor:
R. Yu. Gnizdor, S. Yu. Pridannikov, Vladimir Kim, V. G. Kalyazin, D. V. Merkur’ev, V. S. Zakharchenko
Publikováno v:
Journal of Surface Investigation: X-ray, Synchrotron and Neutron Techniques. 14:1221-1227
We consider the dynamics of local inhomogeneities caused by erosion of the surface of the discharge-chamber walls of a stationary plasma thruster during its prolonged operation. The inhomogeneities lead to the appearance of “longitudinal” (along
Externí odkaz:
https://explore.openaire.eu/search/publication?articleId=doi_________::bab749a922b99e60b5ba2941818d7f8f
https://doi.org/10.1134/s1027451020060087
https://doi.org/10.1134/s1027451020060087
Autor:
G. A. Popov, D. V. Merkur’ev, V. S. Zakharchenko, D. P. Grdlichko, E. A. Shilov, R. Yu. Gnizdor, Vladimir Kim, M. V. Korkunov
Publikováno v:
Cosmic Research. 57:301-309
The paper presents the results of the investigation of the possibility to develop a stationary plasma thruster with increased thrust. This research was carried out by the Research Institute of Applied Mechanics and Electrodynamics, Moscow Aviation In
Externí odkaz:
https://explore.openaire.eu/search/publication?articleId=doi_________::819e7daebbe13f61c81821454afec70e
https://doi.org/10.1134/s0010952519050034
https://doi.org/10.1134/s0010952519050034
Publikováno v:
Plasma Physics Reports. 45:11-20
Morozov’s stationary plasma thrusters (SPTs) operating with xenon have been successfully used for many years in space technology. At the same time, due to the high cost of xenon, interest has arisen in alternate working substances. In a number of w
Externí odkaz:
https://explore.openaire.eu/search/publication?articleId=doi_________::67fbe78a2d634f7e068db0460d0deb20
https://doi.org/10.1134/s1063780x19010082
https://doi.org/10.1134/s1063780x19010082
Autor:
A. N. Kim, A.V. Geliev, D. V. Zhuravlev, A. A. Osika, V. S. Zakharchenko, G. S. Ivanov, A. N. Varyukhin, I.O. Kiselev
Publikováno v:
2021 International Seminar on Electron Devices Design and Production (SED).
The results of temperature-controlled discharge tests of NMC type battery cells of standard size 18,650 are presented. A mathematical model of heat generation rate in a battery cell during its discharge is proposed and substantiated in terms of therm
Externí odkaz:
https://explore.openaire.eu/search/publication?articleId=doi_________::bd90fbf621d90dad726f1ad390fa53c2
https://doi.org/10.1109/sed51197.2021.9444497
https://doi.org/10.1109/sed51197.2021.9444497
Autor:
O. A. Mitrofanova, Vladimir Kim, R. Yu. Gnizdor, V. S. Zakharchenko, D. V. Merkuriev, E. A. Shilov, P. G. Smirnov, D. P. Grdlichko
Publikováno v:
Journal of Surface Investigation: X-ray, Synchrotron and Neutron Techniques. 12:1237-1247
The fundamental principles allowing control of the ionization and acceleration layer position and thickness in the discharge of a stationary plasma thruster (SPT) determining ion flows to the discharge chamber walls and the corresponding energy losse
Externí odkaz:
https://explore.openaire.eu/search/publication?articleId=doi_________::b7cc2cd5fe10a3cd98640b8ed6a0b402
https://doi.org/10.1134/s1027451018050610
https://doi.org/10.1134/s1027451018050610
Autor:
E. A. Shilov, R. Yu. Gnizdor, Vladimir Kim, O. A. Mitrofanova, D. V. Merkur’ev, V. S. Zakharchenko, P. G. Smirnov, D. P. Grdlichko
Publikováno v:
Technical Physics Letters. 44:1108-1110
Requirements for stationary Morozov plasma thrusters are increasing due to the expansion of their use. Therefore, attempts are made to improve the organization of operational processes in the thrusters are undertaken to perfect their characteristics
Externí odkaz:
https://explore.openaire.eu/search/publication?articleId=doi_________::4217370e9789c92355b7da5274f735b2
https://doi.org/10.1134/s1063785018120271
https://doi.org/10.1134/s1063785018120271
Publikováno v:
2019 International Conference on Electrotechnical Complexes and Systems (ICOECS).
The design process of a fuel cell based electric propulsion system an ultralight manned aircraft is presented. Propulsion system consists of electric motor with 60 kW maximum power, 30-35kW proton exchange membrane fuel cell, battery with capacity 1.
Externí odkaz:
https://explore.openaire.eu/search/publication?articleId=doi_________::e62911b1328dae33176f2d6bc744e9aa
https://doi.org/10.1109/icoecs46375.2019.8949950
https://doi.org/10.1109/icoecs46375.2019.8949950
Publikováno v:
2019 International Conference on Electrotechnical Complexes and Systems (ICOECS).
The paper presents an analysis and forecast of the development of hybrid electric and full-electric propulsion systems for an aircraft of different types, key technologies necessary to develop them.
Externí odkaz:
https://explore.openaire.eu/search/publication?articleId=doi_________::cc06fd752676b8dd5f8aec620cc53a7f
https://doi.org/10.1109/icoecs46375.2019.8949910
https://doi.org/10.1109/icoecs46375.2019.8949910
Autor:
D.I. Zhuravlev, A. N. Varyukhin, A.V. Kazakov, I.O. Kiselev, A.V. Geliev, V. S. Zakharchenko, F.A. Zagumennov
Publikováno v:
Journal of Physics: Conference Series. 1891:012013
A description of a full electric propulsion system demonstrator with an energy source based on a battery pack for an ultralight manned Sigma-4 aircraft is presented. The main characteristics and functionality of the main units and devices of the elec
Externí odkaz:
https://explore.openaire.eu/search/publication?articleId=doi_________::6086341c827903877d2df02b6058cd35
https://doi.org/10.1088/1742-6596/1891/1/012013
https://doi.org/10.1088/1742-6596/1891/1/012013