固体火箭推进剂起爆技术  

An experimental research on initiating technique of solid rocket propellant

作　　者：于川[1] 池家春[1] 门举先[1] 仝延锦[1] 桂毓林[1] 张远平[1] 

机构地区：[1]中国工程物理研究院流体物理研究所冲击波物理与爆轰物理实验室,四川绵阳621900

出　　处：《爆炸与冲击》2004年第6期499-502,共4页Explosion and Shock Waves

摘　　要：针对便携式防空导弹的聚醚复合推进剂进行了余药起爆试验。试验表明,在聚能装药起爆器作用下成功地起爆了推进剂药柱。该技术对战斗部 发动机一体化设计有重要应用价值。This paper introduces the initiating experimental study on the remainder of propellant that is made of the ployether composite propellant and used in the portable anti-aircraft missile. Results indicated that the propellants were successfully initiated under the action of the shaped charge. Such a technique could be useful for the application of warhead and engine integral design.

关 键 词：爆炸力学 起爆技术 板痕试验 推进剂 超压 

分 类 号：O381[理学—流体力学]