离子推力器可靠性技术发展思路探讨

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摘要离子推力器的可靠性技术是一项新的研究课题,利用通用和成熟的方法无法准确评价和验证离子推力器的可靠性。本文针对离子推力器工作特点,主要介绍了其可靠性评价、验证以及可靠性增长等技术发展的基本思路。

作者杨福全田华兵董澍贾艳辉龙建飞

机构地区兰州空间技术物理研究所中国航天标准化与产品保证研究院

出处《质量与可靠性》 2014年第5期1-4,46,共5页 Quality and Reliability

关键词离子推力器可靠性技术可靠性评价发展思路

参考文献3

1Zhang Tianping. Initial Flight Test Results of the LIPS-200 Electric Propulsion System on SJ- 9A Satellite [C] . IEPC-2013-47. Washington, D.C. USA.October 6-10, 2013.
2Zhang Tianping. THE LIPS-200 ION ELECTRIC PROPULSION SYSTEM DEVELOPMENT FOR THE DFH-3B SATELLITE PLATFORM [C] IAC-13-C4.4.10. Beijing, CHINA. October 10, 2013.
3贾艳辉,张天平,李小平.离子推力器加速栅寿命的概率性分布和可靠性预测[J].真空与低温,2011,17(2):75-79. 被引量：4

1[JONATHAN L, NOORD V. Lifetime Assessment of the NEXT Ion Thruster[ R]. AIAA 2007-5274.
2IPOLK J E, MOORE N R, Newlin LE, et al. Probabilistic Analysis of Ion Engine Accelerator Grid Life[R]. AIAA 1993-176.
3I BROPHY J R, POLK J E. Ion Engine Service Life Validation by Analysis and Testing[ R]. AIAA 1996-2715.
4PENG X H, RUYTN W M, KEEFER D. Three Dimensional Particle Simulation of Grid Erosion in ion Thruster[ R]. AIAA 1991 -199.
5BROPHY J R, KATZ I, Polk J E, et al. Numerical simulation of ion thruster Accelerator Grid Erosion[ R]. AIAA 2002-4261.
6BROPHY J R, POLK J E. Pless L C. Test-to-failure of a Two-Grid,30-cm-dia. Ion Accelerator System[ R]. IEPC 1993-172.
7RAWLIN V. Internal Erosion Rates of a 10kw Xe Ion Thruster[ R]. AIAA 88-2912.
8JAMES E L, BECHTEL R T. Results of The Mission Profile Life Test First Test Segment: Thruster Jl [ R ], AIAA 1981-0716.
9POLK J E, MOORE N R, BROPI-IY J R, et al. The Role of Analysis and Testing in the service Life Assessment of Ion Engines [S]. IEPC 1995-228.
10BROPHY J R, KATZ I, POLK J E, et al. Numerical Simulation of Ion Thruster Accelerator Grid Erosion [ R ]. AIAA 2002- 4261.

质量与可靠性

2014年第5期

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