火炸药学报2017，Vol.40Issue(6)：7-16,10.DOI:10.14077/j.issn.1007-7812.2017.06.002
复合改性双基推进剂降感技术及感度机理研究进展
Progress of Study on Desensitization Techniques and Sensitivity Mechanisms of Composite Modified Double-base Propellants
摘要
Abstract
Starting from the safety problems faced by high-value weapon platform tactical missiles ,the research pro-gress in the desensitizing techniques and sensitivity mechanisms of composite modified double-base (CMDB) propel-lant energetic components was summarized .From the aspects of modifying /replacing desensitization techniques of energetic filler ,desensitization technique of energetic plasticizers and comprehensive desensitization technique etc ., the matching technique approach between energy and sensitivity of CMDB propellant was summarized .The research work on the sensitivity mechanism of energetic component and multi components in recent years was introduced . The sensitivity mechanism and prediction method of CMDB propellant were summarized .The research trend show that the new insensitive materials and novel desensitization technique should be further applied to CMDB propellants and the sensitivity prediction method should be combined with the theoretical calculation to improve the development efficiency and comprehensive properties of CMDB propellants .With 101 conferences .关键词
改性双基推进剂/CMDB推进剂/钝感高能填料/钝感增塑剂/感度机理/感度预测Key words
composite modified double-base propellants/CMDB propellant/insensitive high energy filler/insensi-tive plasticizers/sensitivity mechanism/prediction of sensitivity分类
军事科技引用本文复制引用
陈京,王晗,刘萌,吴雄岗,樊学忠..复合改性双基推进剂降感技术及感度机理研究进展[J].火炸药学报,2017,40(6):7-16,10.基金项目
国家安全重大基础研究项目 （）
