丁羟推进剂/衬层粘接界面材料力学性能研究  

Research on Mechanical Properties of HTPB Propellant/Liner Bonding Interface

作　　者：李晓光[1] 阳建红[2] 

机构地区：[1]中国人民解放军96451部队 [2]第二炮兵工程学院

出　　处：《化学推进剂与高分子材料》2007年第6期52-55,共4页Chemical Propellants & Polymeric Materials

基　　金：国家973项目;项目名称:固体发动机推进剂/粘接界面失效机理;编号:6133801

摘　　要：比较了目前测试推进剂/衬层粘接界面性能的方法。针对丁羟推进剂/衬层粘接界面,采用国内外关于推进剂与金属材料粘接界面性能的微型拉伸试验方法,设计并开展了微型拉伸试验,得出该推进剂材料在粘接界面处的受影响区域范围及相应的材料性能特征。The present measuring methods of the mechanical properties of the propellant/liner bonding interface are compared. Aiming at the HTPB propellant/liner bonding interface, the tensile test of the microsample was designed and carried out by adopting the studying methods for propellant/metal material bonding interface properties at home and abroad. The affected scope of the propellant in bonding interface, and corresponding material properties were obtained.

关 键 词：端羟基聚丁二烯推进剂 粘接界面 力学性能 衬层 微型拉伸试验 

分 类 号：TB301[一般工业技术—材料科学与工程]