Volume 29 Issue 4
Apr.  2014
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HOU Jin-li, JIN Ping, CAI Guo-biao. Failure mode of reusable rocket engine based on fuzzy fault tree and factor analysis[J]. Journal of Aerospace Power, 2014, 29(4): 987-992. doi: 10.13224/j.cnki.jasp.2014.04.032
Citation: HOU Jin-li, JIN Ping, CAI Guo-biao. Failure mode of reusable rocket engine based on fuzzy fault tree and factor analysis[J]. Journal of Aerospace Power, 2014, 29(4): 987-992. doi: 10.13224/j.cnki.jasp.2014.04.032

Failure mode of reusable rocket engine based on fuzzy fault tree and factor analysis

doi: 10.13224/j.cnki.jasp.2014.04.032
  • Received Date: 2013-01-24
  • Publish Date: 2014-04-28
  • To confirm weak parts of engine and guide the reusable rocket engine reliability design, the key failure mode analysis of major components for space shuttle main engine (SSME) was conducted based on fuzzy fault tree analysis and factor analysis. The result show that the elementary event of highest critical importance is the bearing failure of high-pressure oxidizer turbine pump caused by flaking, pits, wear and corrosion, which is obtained by fuzzy fault tree analysis. The typical failure mode of highest comprehensive factor in engine system is turbine blade failure evaluated by considering risk time, and probability in factor analysis.

     

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