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author V. V. Shalay
V. I. Gorbunkov
I. V. Kolganov
author_facet V. V. Shalay
V. I. Gorbunkov
I. V. Kolganov
author_sort V. V. Shalay
collection DOAJ
description A mathematical model of thermodynamic processes occurring in the arcjet thruster device with using argon for arcjet working process carring out. A comparative analysis of the results of experimental data with theoretical data has been carried out. The purpose of the study is to develop a mathematical model of thermodynamic processes in the arcjet thruster device and simulate the interaction of argon with arc discharge plasma. The comparative analysis of the calculated parameters, thanks to the proximity of electron temperature values with the previously experimentally obtained under the static state in the arcjet thruster device, confirms the reliability of the presented mathematical model of plasma processes and the need for its improvement.
first_indexed 2024-04-14T00:06:18Z
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institution Directory Open Access Journal
issn 2588-0373
2587-764X
language English
last_indexed 2024-04-14T00:06:18Z
publishDate 2022-10-01
publisher Omsk State Technical University, Federal State Budgetary Educational Institution of Higher Education
record_format Article
series Омский научный вестник: Серия "Авиационно-ракетное и энергетическое машиностроение"
spelling doaj.art-eddf54430c3f4aaf92da2e17925bf5772022-12-22T02:23:31ZengOmsk State Technical University, Federal State Budgetary Educational Institution of Higher EducationОмский научный вестник: Серия "Авиационно-ракетное и энергетическое машиностроение"2588-03732587-764X2022-10-0163172310.25206/2588-0373-2022-6-3-17-23Mathematical modeling of plasma thruster device thermal processesV. V. Shalay0https://orcid.org/0000-0003-0635-4849V. I. Gorbunkov1https://orcid.org/0000-0002-5495-5641I. V. Kolganov2Omsk State Technical UniversityOmsk State Technical UniversityJSC «Khrunichev State Research and Production Space Center»A mathematical model of thermodynamic processes occurring in the arcjet thruster device with using argon for arcjet working process carring out. A comparative analysis of the results of experimental data with theoretical data has been carried out. The purpose of the study is to develop a mathematical model of thermodynamic processes in the arcjet thruster device and simulate the interaction of argon with arc discharge plasma. The comparative analysis of the calculated parameters, thanks to the proximity of electron temperature values with the previously experimentally obtained under the static state in the arcjet thruster device, confirms the reliability of the presented mathematical model of plasma processes and the need for its improvement.https://www.omgtu.ru/general_information/media_omgtu/journal_of_omsk_research_journal/files/arhiv/2022/%D0%A2.%206,%20%E2%84%96%203%20(%D0%90%D0%A0%D0%B8%D0%AD%D0%9C)/17-23%20%D0%A8%D0%B0%D0%BB%D0%B0%D0%B9%20%D0%92.%20%D0%92.,%20%D0%93%D0%BE%D1%80%D0%B1%D1%83%D0%BD%D0%BA%D0%BE%D0%B2%20%D0%92.%20%D0%98.,%20%D0%9A%D0%BE%D0%BB%D0%B3%D0%B0%D0%BD%D0%BE%D0%B2%20%D0%98.%20%D0%92..pdfarcjet plasma thrustergas and electron temperaturethermal equilibriumspecific impulseargon plasmathermal model arcjet plasma thruster
spellingShingle V. V. Shalay
V. I. Gorbunkov
I. V. Kolganov
Mathematical modeling of plasma thruster device thermal processes
Омский научный вестник: Серия "Авиационно-ракетное и энергетическое машиностроение"
arcjet plasma thruster
gas and electron temperature
thermal equilibrium
specific impulse
argon plasma
thermal model arcjet plasma thruster
title Mathematical modeling of plasma thruster device thermal processes
title_full Mathematical modeling of plasma thruster device thermal processes
title_fullStr Mathematical modeling of plasma thruster device thermal processes
title_full_unstemmed Mathematical modeling of plasma thruster device thermal processes
title_short Mathematical modeling of plasma thruster device thermal processes
title_sort mathematical modeling of plasma thruster device thermal processes
topic arcjet plasma thruster
gas and electron temperature
thermal equilibrium
specific impulse
argon plasma
thermal model arcjet plasma thruster
url https://www.omgtu.ru/general_information/media_omgtu/journal_of_omsk_research_journal/files/arhiv/2022/%D0%A2.%206,%20%E2%84%96%203%20(%D0%90%D0%A0%D0%B8%D0%AD%D0%9C)/17-23%20%D0%A8%D0%B0%D0%BB%D0%B0%D0%B9%20%D0%92.%20%D0%92.,%20%D0%93%D0%BE%D1%80%D0%B1%D1%83%D0%BD%D0%BA%D0%BE%D0%B2%20%D0%92.%20%D0%98.,%20%D0%9A%D0%BE%D0%BB%D0%B3%D0%B0%D0%BD%D0%BE%D0%B2%20%D0%98.%20%D0%92..pdf
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