摘要
用差示扫描(DSC)和热重分析(TG)研究了斯蒂芬酸铅(LS)/硝化棉(NC)/双铅2(SQ-2)推进剂热稳定性。用热力计算方法分析了四种推进剂(高氯酸铵(AP)/端羟基聚丁二烯(HTPB),AP/NC,LS/NC和LS/SQ-2)的能量特性。研究了配比为55,64,73三种LS/NC推进剂和配比为46,55,64,73四种LS/SQ-2推进剂的热分解特性。结果表明:添加NC或SQ-2能降低LS的热稳定性,提高推进剂的能量,其中NC的效果更显著,认为LS和NC可选作微型发动机用推进剂的组分。
Thermal stabilities of lead styphnate（LS） / nitrocellulose（NC）/ dibasic lead stearate（SQ-2） were studied by Different Scanning Calorimetry（DSC） and Thermogravimetry（TG）.The energetic properties of four propellants（ammonium perchlorate（AP） / hydroxy-terminated polybutadiene（HTPB）,AP/NC,LS/ NC and LS /SQ-2） were analyzed with thermodynamic calculation method.Thermal decomposition characteristics of three LS/NC propellants with ratio of LS to NC as 55,64 and 73 and four LS/SQ-2 propellants with ratio of LS to SQ-2 as 46,55,64 and 73 were researched.Results show that the thermostability of LS decreases by adding NC or SQ-2,and its energy enhances,in which the effect of NC is more obvious,considering that LS and NC can be chosen as the components of propellant used in micro solid rocket motor.
出处
《含能材料》
EI
CAS
CSCD
北大核心
2013年第3期319-324,共6页
Chinese Journal of Energetic Materials
基金
西北工业大学基础研究基金(JC201221)
航天支撑基金(NAXA0003)
关键词
宇航推进理论与工程
热力计算
LS
NC推进剂
热解特性
能量特性
aerospace propulsion theory and engineering
thermodynamic calculation
LS/NC propellant
thermal decomposition characteristic
energy property
作者简介
作者简介：胡松启（1976-），男，副教授，主要从事固体推进剂及燃烧研究。e．mail：13572255355@139．com
