IMECH-IR  > 等离子体与燃烧中心(2009-2011)
Experimental study on energy dissipation in a 1 kW arcjet thruster
Huang HJ(黄河激); Pan WX(潘文霞); Wu CK(吴承康)
会议录名称13th Asian Congress of Fluid Mechanics.Dhaka, Bangladesh.2010-11-17~2010-11-21.
2011-01-06
会议名称13th Asian Congress of Fluid Mechanics
会议日期2010-11-17~2010-11-21
会议地点Dhaka, Bangladesh
摘要As a simple and reliable propulsion system, arcjet thrusters have been used in multiple satellite missions. In order to improve the efficiency of arcjet thrusters, energy dissipation study was carried out in a 1 kW arcjet thruster with pure N2, H2-N2 and H2 as the propellant. Using a 698 nm interference filter, thermal radiation was isolated from arc and plume emissions and the internal nozzle temperature was obtained by converting the thermal radiation signals. Results show that the addition of hydrogen leads to higher nozzle temperature, which is the determining factor for the mode of arc root attachment. At lower nozzle temperatures, constricted type attachment with unstable motions of the arc root was observed, while a fully diffused and stable arc root was observed at elevated nozzle temperatures. Output energy distribution analysis shows that losses from frozen flow and exhaust thermal losses are the main parts in limiting the efficiency of arcjet thrusters.
关键词 arcjet Thruster Performance Energy dissipation
课题组名称LHD应用等离子体力学(CPCR)
收录类别其他
语种中文
文献类型会议论文
条目标识符http://dspace.imech.ac.cn/handle/311007/43278
专题等离子体与燃烧中心(2009-2011)
通讯作者Huang HJ(黄河激)
推荐引用方式
GB/T 7714
Huang HJ,Pan WX,Wu CK. Experimental study on energy dissipation in a 1 kW arcjet thruster[C]13th Asian Congress of Fluid Mechanics.Dhaka, Bangladesh.2010-11-17~2010-11-21.,2011.
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