Volume 30 Issue 10
Oct.  2015
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LI Jun-xing, ZHANG Yong-bo, FU Hui-min, WANG Zhi-hua. Reliability evaluation method of ion thruster withvery few failure data[J]. Journal of Aerospace Power, 2015, 30(10): 2352-2356. doi: 10.13224/j.cnki.jasp.2015.10.008
Citation: LI Jun-xing, ZHANG Yong-bo, FU Hui-min, WANG Zhi-hua. Reliability evaluation method of ion thruster withvery few failure data[J]. Journal of Aerospace Power, 2015, 30(10): 2352-2356. doi: 10.13224/j.cnki.jasp.2015.10.008

Reliability evaluation method of ion thruster withvery few failure data

doi: 10.13224/j.cnki.jasp.2015.10.008
  • Received Date: 2014-04-08
  • Publish Date: 2015-10-28
  • A reliability evaluation method of ion thruster was established under the situation that only two ion thrusters were tested and the results were represented by very few failure data. Meanwhile, the significant test information from the last failure data test to non-occurrence of failure was fully developed by introducing the concept of interval statistic. Best linear unbiased point estimator of the life distribution parameters was calculated by using Gauss-Markov theorem. And then the one-side lower confidence limits of reliability and life were given. At last, while evaluating the reliability of NASA's XIPS-13 ion thrusters, the one-side lower confidence limits of the reliability with the demanding lifetime 10000h was 0.87 and the one-side lower confidence limits of the lifetime with a given reliability 0.9 was 9024.6h. It demonstrates that this method has high accuracy and can be easily applied in engineering.

     

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