Mathematical modeling of plasma thruster device thermal processes

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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Bibliographic Details
Main Authors: V. V. Shalay, V. I. Gorbunkov, I. V. Kolganov
Format: Article
Language:English
Published: Omsk State Technical University, Federal State Budgetary Educational Institution of Higher Education 2022-10-01
Series:Омский научный вестник: Серия "Авиационно-ракетное и энергетическое машиностроение"
Subjects:
arcjet plasma thruster
gas and electron temperature
thermal equilibrium
specific impulse
argon plasma
thermal model arcjet plasma thruster
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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