Arcjet plasma temperature estimation in thruster device
The kinetic theory of gases methods has been used to evaluate plasma arc parameters in the arcjet thruster device. It greatly means the compression process in adiabatic character and gas temperature increasing for excited atoms Boltzmann distribution over the energy levels. Using argon gas for ar...
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| Format: | Article |
| Language: | English |
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Omsk State Technical University, Federal State Autonomous Educational Institution of Higher Education
2018-10-01
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| Series: | Омский научный вестник: Серия "Авиационно-ракетное и энергетическое машиностроение" |
| Subjects: | |
| Online Access: | https://www.omgtu.ru/general_information/media_omgtu/journal_of_omsk_research_journal/files/arhiv/2018/%D0%A2.%202,%20%E2%84%96%203/44-50%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%D1%81%D0%B8%D1%86%D1%8B%D0%BD%20%D0%92.%20%D0%92.,%20%D0%A0%D1%83%D0%B1%D0%B0%D0%BD%20%D0%92.%20%D0%98.,%20%D0%A8%D0%B0%D0%BB%D0%B0%D0%B9%20%D0%92.%20%D0%92..pdf |
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| _version_ | 1832573778178080768 |
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| author | V. I. Gorbunkov V. V. Kositsin V. I. Ruban V. V. Shalay |
| author_facet | V. I. Gorbunkov V. V. Kositsin V. I. Ruban V. V. Shalay |
| author_sort | V. I. Gorbunkov |
| collection | DOAJ |
| description | The kinetic theory of gases methods has been used to evaluate plasma arc parameters in the arcjet thruster
device. It greatly means the compression process in adiabatic character and gas temperature increasing for
excited atoms Boltzmann distribution over the energy levels.
Using argon gas for arcjet working process carring out, the way of gas temperature eveluation is offered.
The results of the study can be use in the spacecraft arcjet development |
| format | Article |
| id | doaj-art-9e10f9d8f2bb4348b1bb76b433087ba2 |
| institution | Kabale University |
| issn | 2588-0373 2587-764X |
| language | English |
| publishDate | 2018-10-01 |
| 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-9e10f9d8f2bb4348b1bb76b433087ba22025-02-02T02:51:15ZengOmsk State Technical University, Federal State Autonomous Educational Institution of Higher EducationОмский научный вестник: Серия "Авиационно-ракетное и энергетическое машиностроение"2588-03732587-764X2018-10-0123445010.25206/2588-0373-2018-2-3-44-50Arcjet plasma temperature estimation in thruster deviceV. I. Gorbunkov0https://orcid.org/0000-0002-5495-5641V. V. Kositsin1V. I. Ruban2V. V. Shalay3https://orcid.org/0000-0003-0635-4849Omsk State Technical UniversityOmsk State Technical UniversityOmsk State Technical UniversityOmsk State Technical UniversityThe kinetic theory of gases methods has been used to evaluate plasma arc parameters in the arcjet thruster device. It greatly means the compression process in adiabatic character and gas temperature increasing for excited atoms Boltzmann distribution over the energy levels. Using argon gas for arcjet working process carring out, the way of gas temperature eveluation is offered. The results of the study can be use in the spacecraft arcjet developmenthttps://www.omgtu.ru/general_information/media_omgtu/journal_of_omsk_research_journal/files/arhiv/2018/%D0%A2.%202,%20%E2%84%96%203/44-50%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%D1%81%D0%B8%D1%86%D1%8B%D0%BD%20%D0%92.%20%D0%92.,%20%D0%A0%D1%83%D0%B1%D0%B0%D0%BD%20%D0%92.%20%D0%98.,%20%D0%A8%D0%B0%D0%BB%D0%B0%D0%B9%20%D0%92.%20%D0%92..pdfarcjet thrusterhigh pressure argon plasmaspecific impulsegas and electron temperaturethe adiabatic character of the compression processlocal thermal equilibriumthe boltzmann distributionemission spectroscopy |
| spellingShingle | V. I. Gorbunkov V. V. Kositsin V. I. Ruban V. V. Shalay Arcjet plasma temperature estimation in thruster device Омский научный вестник: Серия "Авиационно-ракетное и энергетическое машиностроение" arcjet thruster high pressure argon plasma specific impulse gas and electron temperature the adiabatic character of the compression process local thermal equilibrium the boltzmann distribution emission spectroscopy |
| title | Arcjet plasma temperature estimation in thruster device |
| title_full | Arcjet plasma temperature estimation in thruster device |
| title_fullStr | Arcjet plasma temperature estimation in thruster device |
| title_full_unstemmed | Arcjet plasma temperature estimation in thruster device |
| title_short | Arcjet plasma temperature estimation in thruster device |
| title_sort | arcjet plasma temperature estimation in thruster device |
| topic | arcjet thruster high pressure argon plasma specific impulse gas and electron temperature the adiabatic character of the compression process local thermal equilibrium the boltzmann distribution emission spectroscopy |
| url | https://www.omgtu.ru/general_information/media_omgtu/journal_of_omsk_research_journal/files/arhiv/2018/%D0%A2.%202,%20%E2%84%96%203/44-50%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%D1%81%D0%B8%D1%86%D1%8B%D0%BD%20%D0%92.%20%D0%92.,%20%D0%A0%D1%83%D0%B1%D0%B0%D0%BD%20%D0%92.%20%D0%98.,%20%D0%A8%D0%B0%D0%BB%D0%B0%D0%B9%20%D0%92.%20%D0%92..pdf |
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