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离子推力器羽流测量E×B探针设计及误差分析 被引量:11

ANALYSIS AND DESIGN OF E×B PROBE FOR MEASUREMENT OF ION THRUSTER PLUMES
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摘要 分析了E×B探针测量离子电推进羽流的误差,重点讨论了E×B探针的分辨率以及E×B探针设计的主要问题。设计了一种用于离子推力器羽流双荷离子测量的E×B探针。 E×B probe measurement error was analysed. The resolution of the E×B probe and the key problems of design of E×B probe were discussed in detail. A design of E×B probe for measurement of doubly charged ions in ion thruster plumes was presented as well.
机构地区 兰州物理研究所
出处 《真空与低温》 2007年第2期77-80,共4页 Vacuum and Cryogenics
关键词 离子推力器 E×B探针 测量误差 羽流 ion thruster E×B probe measurement error plume
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参考文献6

  • 1SANG-WOOK KIM,Ph.D.Thesis,Experimental investigations of plasma parameters and species-dependent Ion energy distribution in the plasma exhaust plume of a Hall Thruster[D].University of Michigan,Department of Aerospace Engineering,1999. 被引量:1
  • 2MITCHELL LOUIS RONALD WALKER,Ph.D.Thesis,Effects of facility backpressure on the performance and plume of a Hall Thruster[D].University of Michigan,Department of Aerospace Engineering,2005. 被引量:1
  • 3RICHARD ROBERT HOFER,Ph.D.Thesis,The development and characterization of High-efficiency,High-specific Impulse Xenon Hall Thruster[D].University of Michigan,Department of Aerospace Engineering,2004. 被引量:1
  • 4PETER YOUNG PETERSON,Ph.D.Thesis,The development and characterization of a two-stage Hybrid Hall/Ion Thruster[D].University of Michigan,Department of Aerospace Engineering,2004. 被引量:1
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二级参考文献3

  • 1GEORGE C SOULAS, JOHNE FOSTER, MICHAEL J, et al. Performance of titanium optics on a NASA 30 cm ion thruster [ R]. AIAA-2000-3814, 2000. 被引量:1
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  • 3KING H J. Low Voltage 30 - cm Ion Thruster Development [ R ]. NASA, CR- 134731,1974. 被引量:1

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