航天推进技术研究院主办
ZHANG Yan,KANG Xiao-lu.Experimental investigation on plasma discharge modes of BaW hollow cathode[J].Journal of Rocket Propulsion,2013,39(01):29-35.
钡钨空心阴极等离子体放电模式实验研究
- Title:
- Experimental investigation on plasma discharge modes of BaW hollow cathode
- Keywords:
- BaW hollow cathode; plasma discharge; discharge mode
- 分类号:
- V439-33
- 文献标志码:
- A
- 摘要:
- 主要通过实验的手段,系统研究了钡钨空心阴极的等离子体放电特性及其工作模式。实验中,使空心阴极工作在三极管构型下,调节相应的放电参数,详细分析钡钨空心阴极放电特性的变化规律、存在的放电模式及其转化规律。最后得到结论:钡钨空心阴极放电表现为羽毛状、亮斑状和弥漫状等3种典型的工作模式;不同放电模式可以用放电电流、放电电压及其振荡特性进行判定和区分;随着放电参数的变化,几种放电模式之间可以相互转化。
- Abstract:
- The plasma discharge characteristics and different discharge modes of BaW hollow cathode are systematically studied via experiment in this paper. During the experiment, the relevant discharge parameters of hollow cathode working in triode configuration were adjusted, and the discharge characteristics, the possible discharge modes and the transition between different discharge modes of BaW hollow cathode were analyzed in detail. The conclusions that the BaW Hollow ca- thode has three distinct discharge modes (plume mode, spot mode and diffuse mode) were acquired at the end. The three modes can be clearly distinguished by the change of discharge current, discharge voltage and their oscillation characteristics. Furthermore, the transition among the three modes can be realized as the discharge parameter changes.
参考文献/References:
[1]SAKAI S, KATAYAMA T. Discharge modes and characteris- tics of hollow cathode[C]// The 30th Inter- national Elec- tric Propulsion Conference. Florence, Italy: IEPC, 2007: 1-7.
[2]张天平, 袁子, 田华兵. 电推进系统空心阴极研制试验技术[J]. 真空电子技术, 2007 (2): 9-13.
[3]KAMHAWI H, PATTERSON M J. On the opera- tional status of the international space station plasma con- tactor hollow cathodes, AIAA2005-3676[R]. USA: AIAA, 2005.
[4]孙宗祥. 等离子体减阻技术的研究进展[J]. 力学进展,2003, 33(1): 87-94.
[5]方绍强, 赵尚弘, 余侃民, 等. 飞行器等离子体隐身技术[J]. 现代防御技术, 2005, 33(2): 32-35.
[6]于志强, 李季, 邵文生. 应用于离子发动机和霍尔推力器的空心阴极组件的研究[C]. 北京真空电子技术研究所, 第十七届中国电子学会真空电子学分会年会军用微波管研讨会论文集(下). 2009.
[7]MANDELL M J, KATZ I. Theory of hollow cathode opera- tion in spot and plume modes, AIAA 94-3134[R]. USA: AIAA, 1994.
[8]DOMONKOS M T, GALLIMORE A D, PAT TERSON M J. An evaluation of hollow cathode scal- ing to very low power and flow rate[C]// The 25th Interna- tional Electric Propulsion Conference. Cleveland, OH, US: IEPC, 1997: 121-129.
[9]NISHIYAMA K, SHIMIZU H, FUNAKI K. EMI of mi- crowave discharge neutralizer and hollow cathode[C]// Ab- stracts of ISAS Space Transport Symposium. Japan: ISAS, 2001: 211-218.
[10]YOSHIDA H. Four-step double sheath model of a neu- tralizer hollow cathode[C]// 48th Space Sciences and Tech- nology Conference. Fukui, Japan: SSTC, 2004: 4-6.
[11]PATTERSON S W, MALIK A K. Noise and os- cillatory disturbances in the t6 ion thruster hollow cath- ode, AIAA 99-2577[R]. USA: AIAA, 1999.
相似文献/References:
[1]张 岩,康小录,乔彩霞.钡钨空心阴极放电等离子体特性实验研究[J].火箭推进,2014,40(05):55.
ZHANG Yan,KANG Xiao-lu,QIAO Cai-xia.Experimental investigation for discharge plasma
properties of BaW hollow cathode[J].Journal of Rocket Propulsion,2014,40(01):55.
备注/Memo
收稿日期:2012-03-07;修回日期:2012-05-06 作者简介:张岩(1976—),男,工程师,研究领域为航天发动机测控技术