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电推进系统空心阴极研制试验技术 被引量：7

Development Tests of Hollow Cathodes for Electric Propulsion
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摘要 空心阴极是电推进系统可靠性和工作寿命关键部件,空心阴极研制在很大程度上依赖于阴极试验技术的支持。本文从空心阴极的试验分类、试验设备、试验技术等方面介绍了电推进系统应用空心阴极的研制试验技术。 Hollow cathodes are key assemblies of reliability and life for an electric propulsion system,and their developments are strongly depended on a series of tests.In this paper,the development tests of a hollow cathode for ion or hall thruster was presented within three aspects,including test kinds,test facilities,and test technologies,respectively.
作者 张天平 袁子 田华兵
机构地区 兰州物理研究所
出处 《真空电子技术》 2007年第2期9-14,共6页 Vacuum Electronics
关键词 空心阴极 电推进 研制试验 寿命试验 Hollow cathode Electric propulsion Development test Life test
分类号 O462 [理学—电子物理学]
  • 相关文献

参考文献20

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  • 2[2]Van-Noord J L,Kamhawi H,Mcewen H K.Characterization of a High Current,Long Life Hollow Cathode[R].NASA/TM-2006-214095,2006.
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  • 4[4]Rovey J L,Gallimore A D.Dormant Cathode Plasma Properties and Erosion Analysis in a Multiple-Cathode,High-Power,Rectangular Discharge Chamber[R].AIAA 2005-4241,2005.
  • 5张天平.国外离子和霍尔电推进技术最新进展[J].真空与低温,2006,12(4):187-193. 被引量：66
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  • 7[7]Sengupta A,Brophy J R.,Goodfellow K D.An Over view of the Results from the 30,000 Hr Life Test of Deep Space 1 Flight Spare Ion Engine[R].AIAA-2004-3608,2004.
  • 8[8]Sengupta A.Destructive Physical Analysis of Hollow Cathodes from the Deep Space 1 Flight Spare Ion Engine 30,000 Hr Life Test[R].IEPC-2005-026,2005.
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二级参考文献33

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共引文献65

同被引文献67

  • 1张天平,唐福俊,田华兵.国外电推进系统空心阴极技术[J].上海航天,2008,25(1):39-46. 被引量：8
  • 2方绍强,赵尚弘,余侃民,刘涛.飞行器等离子体隐身技术[J].现代防御技术,2005,33(2):32-35. 被引量：8
  • 3郭宁,江豪成,高军,聂文虎.离子发动机空心阴极失效形式分析[J].真空与低温,2005,11(4):239-242. 被引量：17
  • 4Jacobson D T, John J, Kamhawi H, et al. An Overview of Hall Thruster Development at NASA's John H. Glenn Research Center[R]. AIAA 2005-4242.
  • 5Van-Noord J L, Kamhawi H, Mcewen H K. Characterization of a High Current, Long Life Hollow Cathode [R]. NASA/TM 2006-214095.
  • 6Randolph T, Polk J. An Overview of the Nuclear Electric Xenon Ion System (NEXIS) Activity [R]. AIAA 2004-3450.
  • 7Rovey J L, Gallimore A D. Dormant Cathode Plasma Properties and Erosion Analysis in a Multiple-Cathode, High-Power, Rectangular Discharge Chamber [R]. AIAA 2005-4241.
  • 8Polk J E, Kakuda R Y, Brinza D, et al. Demonstration of the NSTAR Ion Propulsion System on the Deep Space One Mission[R]. IEPC 2001-075.
  • 9Sengupta A, Brophy J R., Goodfellow K D. An Overview of the Results from the 30,000 Hr Life Test of Deep Space 1 Flight Spare Ion Engine[R]. AIAA 2004-3608.
  • 10Sengupta A. Destructive Physical Analysis of Hollow Cathodes from the Deep Space 1 Flight Spare Ion Engine 30,000 Hr Life Test[R]. IEPC 2005-026.

引证文献7

二级引证文献21

真空电子技术
2007年 第2期

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