Mathematical modeling of plasma thruster device thermal processes

Authors

DOI:

https://doi.org/10.25206/2588-0373-2022-6-3-17-23

Keywords:

arcjet plasma thruster, gas and electron temperature, thermal equilibrium, specific impulse, argon plasma, thermal model arcjet plasma thruster

Abstract

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.

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Author Biographies

Victor Vladimirovich Shalay, Omsk State Technical University, Omsk, Russia

Doctor of Technical Sciences, Professor, Head of Transport, Oil and Gas Storage, Standardization and Certification Department, President, Omsk State Technical University (OmSTU), Omsk.

Vladimir Ivanovich Gorbunkov, Omsk State Technical University, Omsk, Russia

Candidate of Physico-Mathematical Sciences, Associate Professorof Theoretical and General Electrical Engineering Department, Head of Photonics and gas discharges spectroscopy Laboratory, OmSTU, Omsk.

Ivan Veniaminovich Kolganov, JSC «Khrunichev State Research and Production Space Center», Russia, Moscow

Design Engineer category 2, JSC «Khrunichev State Research and Production Space Center», Moscow.

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Abstract views: 40

Published

2022-10-13

How to Cite

Shalay В. В., Gorbunkov В. И., & Kolganov И. В. (2022). Mathematical modeling of plasma thruster device thermal processes. Omsk Scientific Bulletin. Series «Aviation-Rocket and Power Engineering», 6(3), 17–23. https://doi.org/10.25206/2588-0373-2022-6-3-17-23

Issue

Vol. 6 No. 3 (2022)

Section

Power and chemical engineering

License

Non-exclusive rights to the article are transferred to the journal in full accordance with the Creative Commons License BY-NC-SA 4.0 «Attribution-NonCommercial-ShareAlike 4.0 Worldwide License (CC BY-NC-SA 4.0»)

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