Global Modeling of N2O Discharges: Helicon Plasma Thruster Application

A global (volume averaged) model pertaining to N2O discharges is used to design and to study electric propulsion applications, especially helicon plasma thrusters fed with pure N2O and also with N2/O2 mixtures including air. Results obtained for N2O feeding are discussed and compared to those pertai...

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Main Authors: Konstantinos Katsonis, Chloe Berenguer
Format: Article
Language:English
Published: Wiley 2013-01-01
Series:International Journal of Aerospace Engineering
Online Access:http://dx.doi.org/10.1155/2013/467503
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author Konstantinos Katsonis
Chloe Berenguer
author_facet Konstantinos Katsonis
Chloe Berenguer
author_sort Konstantinos Katsonis
collection DOAJ
description A global (volume averaged) model pertaining to N2O discharges is used to design and to study electric propulsion applications, especially helicon plasma thrusters fed with pure N2O and also with N2/O2 mixtures including air. Results obtained for N2O feeding are discussed and compared to those pertaining to an air-like N2/O2 mixture feeding. An interesting similarity is observed. Comparison of the N2O model results versus those of Ar shows lower ionization percentage with higher electron temperature for N2O propellant.
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institution Kabale University
issn 1687-5966
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language English
publishDate 2013-01-01
publisher Wiley
record_format Article
series International Journal of Aerospace Engineering
spelling doaj-art-c8d84ddc1ca247e7bac55c71c8ff86382025-08-20T03:24:08ZengWileyInternational Journal of Aerospace Engineering1687-59661687-59742013-01-01201310.1155/2013/467503467503Global Modeling of N2O Discharges: Helicon Plasma Thruster ApplicationKonstantinos Katsonis0Chloe Berenguer1DEDALOS Ltd., Vassilissis Olgas 128, 54645 Thessaloniki, GreeceDEDALOS Ltd., Vassilissis Olgas 128, 54645 Thessaloniki, GreeceA global (volume averaged) model pertaining to N2O discharges is used to design and to study electric propulsion applications, especially helicon plasma thrusters fed with pure N2O and also with N2/O2 mixtures including air. Results obtained for N2O feeding are discussed and compared to those pertaining to an air-like N2/O2 mixture feeding. An interesting similarity is observed. Comparison of the N2O model results versus those of Ar shows lower ionization percentage with higher electron temperature for N2O propellant.http://dx.doi.org/10.1155/2013/467503
spellingShingle Konstantinos Katsonis
Chloe Berenguer
Global Modeling of N2O Discharges: Helicon Plasma Thruster Application
International Journal of Aerospace Engineering
title Global Modeling of N2O Discharges: Helicon Plasma Thruster Application
title_full Global Modeling of N2O Discharges: Helicon Plasma Thruster Application
title_fullStr Global Modeling of N2O Discharges: Helicon Plasma Thruster Application
title_full_unstemmed Global Modeling of N2O Discharges: Helicon Plasma Thruster Application
title_short Global Modeling of N2O Discharges: Helicon Plasma Thruster Application
title_sort global modeling of n2o discharges helicon plasma thruster application
url http://dx.doi.org/10.1155/2013/467503
work_keys_str_mv AT konstantinoskatsonis globalmodelingofn2odischargesheliconplasmathrusterapplication
AT chloeberenguer globalmodelingofn2odischargesheliconplasmathrusterapplication