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胶接法修补固体发动机药柱裂纹技术

Adhesive repair technique for grain crack of solid rocket motor

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【作者】 卢明章谢丽宽马拯

【Author】 LU Ming-zhang1,XIE Li-kuan2,MA Zheng3(1.College of Astronautics,Northwestern Polytechnical University,Xi’an 710072,China;2.Military Representatives Office of NDMMP in Xi’an,Xi’an 710025,China;3.School of Astronautics,Beijing University of Aeronautics and Astronautics,Beijing 100083,China)

【机构】 西北工业大学航天学院海军驻西安地区导弹发动机专业军事代表室北京航空航天大学宇航学院 西安710072西安710025北京100083

【摘要】 使用胶粘剂对固体发动机药柱裂纹实施修补,通过单向拉伸试验测定修补区域药柱的力学性能来验证修补的有效性,并使用高温加速老化预测药柱修补区域的贮存寿命;进行了发动机药柱结构完整性分析,比照试验数据和理论计算结果,证明胶接法可对发动机药柱裂纹实施有效修补。

【Abstract】 The cracks of solid motor grain were repaired by means of the adhesive.Mechanical properties of the repaired grain were measured by the unidirectional tensile test,and the results show that the repair work is effective.The service life of the repaired region of grain was predicted by high-temperature acceleration aging test.The structural integrity of SRM grain was analyzed;the test data were compared with the theoretical calculation results,and the results show that the adhesive repair method for motor grain is very effective.

【关键词】 固体推进剂裂纹修补胶接结构完整性
【Key words】 solid propellantcrackrepairadhesivestructural integrity
  • 【文献出处】 固体火箭技术 ,Journal of Solid Rocket Technology , 编辑部邮箱 ,2007年04期
  • 【分类号】V512
  • 【被引频次】1
  • 【下载频次】92
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