Global Modeling of N2O Discharges: Helicon Plasma Thruster Application

被引：1
|
作者：
Katsonis, Konstantinos [1 ]
Berenguer, Chloe [1 ]
机构：
[1] DEDALOS Ltd, Thessaloniki 54645, Greece
来源：
INTERNATIONAL JOURNAL OF AEROSPACE ENGINEERING | 2013年 / 2013卷
关键词：
D O I：
10.1155/2013/467503
中图分类号：
V [航空、航天];
学科分类号：
08 ; 0825 ;
摘要：
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 N-2/O-2 mixtures including air. Results obtained for N2O feeding are discussed and compared to those pertaining to an air-like N-2/O-2 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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页数：9
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