Arcjet plasma temperature estimation in thruster device

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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Bibliographic Details
Main Authors: V. I. Gorbunkov, V. V. Kositsin, V. I. Ruban, V. V. Shalay
Format: Article
Language:English
Published: Omsk State Technical University, Federal State Autonomous Educational Institution of Higher Education 2018-10-01
Series:Омский научный вестник: Серия "Авиационно-ракетное и энергетическое машиностроение"
Subjects:
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
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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