global modeling of n2o discharges: helicon plasma thruster application
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ID: 168246
2013
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Abstract
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.
| Reference Key |
katsonis2013internationalglobal
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|---|---|
| Authors | ;Konstantinos Katsonis;Chloe Berenguer |
| Journal | shanghai kou qiang yi xue = shanghai journal of stomatology |
| Year | 2013 |
| DOI |
10.1155/2013/467503
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