含硼推进剂一次燃烧固相产物氧化反应特性  

Oxidation Characteristics of Solid Phase Primary Combustion Products of Boron-Based Propellants

作　　者：梁导伦 刘建忠[1] 陈冰虹[1] 李和平[1,2] 周俊虎[1] 

机构地区：[1]浙江大学能源清洁利用国家重点实验室,浙江杭州310027 [2]杭州电子科技大学能源研究所,浙江杭州310018

出　　处：《推进技术》2017年第4期948-953,共6页Journal of Propulsion Technology

基　　金：国家自然科学基金(51106135)

摘　　要：对硼基推进剂一次燃烧固相产物进行研究,是获得硼基推进剂二次燃烧氧化特性的重要手段。为比较在硼基推进剂初始配方中添加KClO_4和CL-20两种含氧添加剂对其二次燃烧氧化特性的影响,通过场发射扫描电镜、常压热分析系统和自主研发的激光点火试验系统对硼基推进剂一次燃烧固相产物样品进行了试验研究。结果表明,样品的热氧化过程主要包含三次失重过程和一次增重过程。先后经历了H_3BO_3分解析出的水分蒸发、NH_4Cl分解、C和B_mC_n氧化、B的氧化过程。在硼基推进剂初始配方中使用CL-20代替KClO_4,可使样品的放热量由7.62kJ/g提升到8.33kJ/g。样品的激光点火燃烧过程中可以观察到B,C两种元素的特征光谱。添加了KClO_4的样品中还能观察到KCl的特征光谱。在硼基推进剂中添加CL-20比添加KClO_4更有利于其一次燃烧固相产物的点火和自持燃烧,可使其二次燃烧的平均燃烧温度由1512°C提升到1633°C。Study on istics of the boron-based primary combustion products is important to obtain the secondary combustion character- propellant. To compare the secondary combustion characteristics of boron-based propel- lants with different oxidizers （KCIO4 and CL-20）, two primary combustion products were studied using a field emission scanning electron microscope, a thermogravimetric balance, and a laser ignition experimental system. Results indicate that the thermal oxidation process of the samples mainly contain three mass loss stages and one mass gain stage. Tile water evaporation caused by decomposition and precipitation of H3BO3, NH4C1 decomposi- tion, C oxidation, BaCh oxidation, and B oxidation processes taken place successively. The heat release of the sample can be enhanced from 7620J/g to 8333 J/g by adding CL-20 instead of KC104 in the original formula of bo- ron-based propellant. Characteristic spectra of B and C elements were observed in laser ignition and combustion processes of both samples. The characteristic spectrum of KCI was also observed in combustion process of the sample with KCIO4. CL-20 has better influence on the ignition and combustion of the primary combustion prod- ucts than KClO4, and can increase the average combustion temperature from 1512 ℃ to 1633 ℃.

关 键 词：硼基推进剂 二次燃烧 含氧添加剂 热氧化 激光点火燃烧 

分 类 号：TJ55[兵器科学与技术—军事化学与烟火技术] V512[航空宇航科学与技术—航空宇航推进理论与工程]