Volt-ampere characteristics, nozzle temperature and thruster performances in a low power argon arcjet
文献类型:会议论文
作者 | Pan WX(潘文霞)![]() ![]() ![]() |
出版日期 | 2011-01-12 |
会议名称 | 13th Asian Congress of Fluid Mechanics |
会议日期 | 2010-12-17~2010-12-21 |
会议地点 | Dhaka, Bangladesh |
通讯作者邮箱 | wxpan@imech.ac.cn |
关键词 | eywor arcjet thruster, volt-ampere characteristics, nozzle temperature |
通讯作者 | 潘文霞 |
中文摘要 | Argon gas with simple atomic structure and favorite arcing stability at low input power was used as the propellant. The thruster with a regeneratively cooled nozzle were tested in a vacuum system capable of keeping the chamber pressure at about 10 Pa at a propellant feeding rate of 5 slm. Arc current, arc voltage, thrust, nozzle temperature and propellant feeding rate were measured in situ simultaneously. Effects of the working parameters such as the propellant feeding rate and arc current on the thruster performances, mainly the produced thrust, specific impulse and thrust efficiency, were examined. The variation of arc volt-ampere characteristics with running time and the effect of nozzle temperature on thruster property are discussed. |
收录类别 | 其他 |
合作状况 | 国际 |
会议录 | 13th Asian Congress of Fluid Mechanics. Dhaka, Bangladesh.2010-12-17~2010-12-21.
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学科主题 | 电磁流体力学和等离子体动力学 |
语种 | 英语 |
源URL | [http://dspace.imech.ac.cn/handle/311007/43295] ![]() |
专题 | 力学研究所_等离子体与燃烧中心(2009-2011) |
推荐引用方式 GB/T 7714 | Pan WX,Meng X,Wu CK. Volt-ampere characteristics, nozzle temperature and thruster performances in a low power argon arcjet[C]. 见:13th Asian Congress of Fluid Mechanics. Dhaka, Bangladesh. 2010-12-17~2010-12-21. |
入库方式: OAI收割
来源:力学研究所
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