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NEPE推进剂/衬层粘接界面细观力学性能/结构研究
引用本文:吴丰军,彭松,池旭辉.NEPE推进剂/衬层粘接界面细观力学性能/结构研究[J].固体火箭技术,2010,33(1).
作者姓名:吴丰军  彭松  池旭辉
作者单位:中国航天科技集团公司四院四十二所,襄樊,441003
摘    要:研究了不同组成的NEPE推进剂/衬层粘接界面细观力学性能和结构的差异,以及对应粘接界面贮存过程中粘接性能和破坏方式的变化规律,探索了粘接界面的细观力学性能、结构与破坏方式的内在关联,初步提出NEPE推进剂/衬层粘接界面失效模式。试验结果表明,粘接界面细观力学性能、结构与界面粘接质量相关,是影响界面失效模式的主要因素。粘接界面具有高模量、高硬度层,N元素含量高且有明显梯度变化时,粘接质量较好,发生内聚破坏,反之发生界面破坏或混合破坏;老化过程中,粘接界面的模量和硬度降低、N元素的含量明显降低决定粘接界面依次发生内聚破坏、混合破坏和界面破坏。

关 键 词:NEPE推进剂  界面  模量  硬度  结合能  

Study on microcosmic mechanics performance/structure of NPPE propellant/liner bonded interface
WU Feng-jun,PENG Song,CHI Xu-hui.Study on microcosmic mechanics performance/structure of NPPE propellant/liner bonded interface[J].Journal of Solid Rocket Technology,2010,33(1).
Authors:WU Feng-jun  PENG Song  CHI Xu-hui
Institution:The 42nd Institute of the Fourth Academy of CASC;Xiangfan 441003;China
Abstract:The diversities of microcosmic mechanical performance/structure in different bonded interface of NEPE propellant/liner and the rule of bonded performance and breakage modes were studied.The inhesion correlations between microcosmic mechanical performance/structure with breakage mode were researched.The prelimary failure mode of NEPE propellant/liner was put forward.The experimental results show that microcosmic mechanical performance/structure has inhesion correlation with the quality of interface and it is...
Keywords:NEPE propellant  interface  modulus  hardness  bonding energy  
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