Automated test bench for simulation of radiation electrification of spacecraft structural dielectrics; IOP Conference Series: Materials Science and Engineering; Vol. 168 : Radiation-Thermal Effects and Processes in Inorganic Materials (RTEP2016)

Bibliografski detalji
Parent link:IOP Conference Series: Materials Science and Engineering
Vol. 168 : Radiation-Thermal Effects and Processes in Inorganic Materials (RTEP2016).— 2017.— [012037, 6 p.]
Autor kompanije: Национальный исследовательский Томский политехнический университет (ТПУ) Институт физики высоких технологий (ИФВТ) Кафедра сильноточной электроники (СЭ)
Daljnji autori: Vladimirov A. M. Aleksandr Mikhailovich, Bezhayev A. Yu., Zykov V. M. Vladimir Mikhailovich, Isaychenko V. I. Vadim Igorevich, Lukashchuk A. A. Andrei Aleksandrovich, Lukonin S. E. Stanislav Evgenievich
Sažetak:Title screen
The paper describes the test bench "Prognoz-2" designed in Testing Center, Institute of Non-Destructive Testing, Tomsk Polytechnic University, which can be used: for ground testing of individual samples of spacecraft structural materials (e.g. thermal control coatings or cover glasses for solar batteries) or ceramics of the plasma thruster discharge channel), and whole spacecraft units or instruments (e.g. instruments of solar and stellar orientation or correcting plasma thrusters) exposed to radiation electrification factors; to verify the calculation mathematical models of radiation electrification of structural dielectrics under the impact of space factors in different orbits.
Jezik:engleski
Izdano: 2017
Serija:Physical and chemical phenomena in inorganic materials in radiation, electrical and thermal fields
Teme:
Online pristup:http://dx.doi.org/10.1088/1757-899X/168/1/012037
http://earchive.tpu.ru/handle/11683/37754
Format: Elektronički Poglavlje knjige
KOHA link:https://koha.lib.tpu.ru/cgi-bin/koha/opac-detail.pl?biblionumber=653811

MARC

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330 |a The paper describes the test bench "Prognoz-2" designed in Testing Center, Institute of Non-Destructive Testing, Tomsk Polytechnic University, which can be used: for ground testing of individual samples of spacecraft structural materials (e.g. thermal control coatings or cover glasses for solar batteries) or ceramics of the plasma thruster discharge channel), and whole spacecraft units or instruments (e.g. instruments of solar and stellar orientation or correcting plasma thrusters) exposed to radiation electrification factors; to verify the calculation mathematical models of radiation electrification of structural dielectrics under the impact of space factors in different orbits. 
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463 0 |0 (RuTPU)RU\TPU\network\19289  |t Vol. 168 : Radiation-Thermal Effects and Processes in Inorganic Materials (RTEP2016)  |o XII International Conference, 4–12 September 2016, Tomsk, Russian Federation  |o [proceedings]  |v [012037, 6 p.]  |d 2017 
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701 1 |a Bezhayev  |b A. Yu. 
701 1 |a Zykov  |b V. M.  |c Physicist, Specialist in the field of quality  |c Professor of Tomsk Polytechnic University, Doctor of technical sciences  |f 1940-  |g Vladimir Mikhailovich  |3 (RuTPU)RU\TPU\pers\38201  |9 20690 
701 1 |a Isaychenko  |b V. I.  |c specialist in the field of non-destructive testing  |c laboratory assistant of Tomsk Polytechnic University  |f 1994-  |g Vadim Igorevich  |3 (RuTPU)RU\TPU\pers\35071 
701 1 |a Lukashchuk  |b A. A.  |c Physicist  |c Leading engineer of Tomsk Polytechnic University  |f 1966-  |g Andrei Aleksandrovich  |3 (RuTPU)RU\TPU\pers\38202 
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