Mathematical modeling of plasma thruster device thermal processes
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 mathemat...
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| Format: | Article |
| Language: | English |
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Omsk State Technical University, Federal State Autonomous Educational Institution of Higher Education
2022-10-01
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| Series: | Омский научный вестник: Серия "Авиационно-ракетное и энергетическое машиностроение" |
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| Online Access: | 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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| _version_ | 1832572978290753536 |
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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. |
| format | Article |
| id | doaj-art-eddf54430c3f4aaf92da2e17925bf577 |
| institution | Kabale University |
| issn | 2588-0373 2587-764X |
| language | English |
| publishDate | 2022-10-01 |
| publisher | Omsk State Technical University, Federal State Autonomous Educational Institution of Higher Education |
| record_format | Article |
| series | Омский научный вестник: Серия "Авиационно-ракетное и энергетическое машиностроение" |
| spelling | doaj-art-eddf54430c3f4aaf92da2e17925bf5772025-02-02T06:08:41ZengOmsk State Technical University, Federal State Autonomous 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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