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XXII межвузовская молодежная научная школа-конференция имени Б. С. Ишханова Концентрированные потоки энергии в космической технике
2021.
Valentin A.
In press
Language:
Russian
Valentin A., Tyryshkina Y., , in : 2019 International Seminar on Electron Devices Design and Production (SED). : IEEE, 2019.
Nowadays, much attention is paid to research in the field of internal electrification of spacecraft (ES). It was shown that the ability of dielectrics to prevent the occurrences of electrostatic discharges (ESD) is determined by their conductivity, which is vary greatly during ground tests and under the influence of space factors. In this article, an ...
Added: August 19, 2022
V.S. Saenko, A.P. Tyutnev, M.A. Afanasyeva et al., IEEE Transactions on Plasma Science 2019 Vol. 47 No. 8 P. 3648-3652
Abstract—We have simulated an electron bulk charging of the plastic cases of electronic devices as an integral part of the spacecraft internal charging problem. The semiconductor crystal has been placed inside a spherical shell of a polymer dielectric 10^−3–10^−2 m thick having an intrinsic (dark) conductivity in the range from 10^−16 to 10^−9 Ohm
^−1 ·m^−1. The crystal itself is a parallelepiped ...
Added: February 3, 2019
Valentin A., [б.и.], 2021
About charge carrier mobility in common insulating polymers ...
Added: May 23, 2022
Novikov L., Makletsov A. A., Sinolits V. V., Advances in Space Research (includes Cospar Information Bulletin) 2016 Vol. 57 No. 2 P. 671-680
In the paper, we discuss numerical modeling of spacecraft charging in geosynchronous orbit which was done using Coulomb-2, NASCAP-2K and SPIS codes, and present data obtained using the MUSCAT code too. The main distinctive features of the codes above are specified, description of the Coulomb-2 code is given in more details. We compare the results ...
Added: January 27, 2017
Belik G. A., Saenko V. S., Abrameshin A. E., В кн. : Труды XXIII Международной конференции "Радиационная физика твердого тела" (Севастополь, 8 июля - 13 июля 2013). : М. : ФГБНУ "НИИ ПМТ", 2013. С. 440-446.
Описывается новый метод повышения устойчивости бортовой аппаратуры к факторам внутренней электризации путем использования слабопроводящего диалектрика. На примере модельного диэлектрика показана такая возможность. Экспериментально измерены его электрофизические характеристики. По разработанной методике проведена оценка его электризуемости. Обсуждаются полученные результаты. ...
Added: November 13, 2013
Belik G. A., Abrameshin A. E., Saenko V. S., Технологии электромагнитной совместимости 2012 № 3(42) С. 5-16
A review of the literature on internal electrification onboard avionics spacecraft. The influence of space weather on the degree of electrification of the spacecraft. The main responses to the factors affecting the electrification. ...
Added: November 8, 2012
Afanasyeva M., , in : 2019 International Seminar on Electron Devices Design and Production (SED). : IEEE, 2019.
The paper presents the results of air
penetration strength experimental studies for a
two-electrode system consisting of a small radius and
plane hemispheres as the method of technical equipment
testing for determining their resistance to electrostatic
discharges. The hemisphere radius is much smaller than
the distance between the electrodes, so the mathematical
expression is used since the 50s of the last for ...
Added: July 25, 2019
Tyutnev A., М. : Московский государственный институт электроники и математики, 2012
Tyutnev A.P. T 98 The processes of electron charging of dielectrics the electronic devices in the space environment. Textbook. Mosk. State. Inst. of Electronics and Mathematics. M., 2012. 56c. ISBN 978-5-94506-336-5 We will discuss general patterns of occurrence of the electric fields in dielectrics electronic means in the space environment when they are irradiated by ...
Added: April 24, 2013
Novikov L., Makletsov A. A., Sinolits V. V., IEEE Transactions on Plasma Science 2017 Vol. 45 No. 8 P. 1919-1922
Influence of electric field of charged spacecraft on secondary emission currents on the spacecraft surface is analyzed in terms of computation of secondary electron trajectories. Dependencies of the recollected electrons number on the electric field intensity at various distances from the emission point for standard secondary electron spectra are calculated. Criteria of the secondary electron ...
Added: January 24, 2018
Novikov L., Makletsov A. A., Sinolits V. V., IEEE Transactions on Plasma Science 2017 Vol. 45 No. 8 P. 1915-1918
This paper describes modeling of spacecraft charging dynamics which is used in COULOMB-2 code in the case of spacecraft surface complex shape. The modeling of spacecraft charging is carried out via numerically solving the system of differential equations for time variations of local electric charge on every discrete element of the spacecraft surface. The presented ...
Added: January 19, 2018