期刊文献+
共找到2篇文章
< 1 >
每页显示 20 50 100
Synthesis of multifunctional additives for solid propellants:Structure,properties and mechanism
1
作者 Pingan Zhang Lina Sun +1 位作者 Jianmin Yuan Jianru Deng 《Defence Technology(防务技术)》 SCIE EI CAS CSCD 2024年第3期308-316,共9页
To simplify the composite propellant formulation and address the current issue of the single-functionality present in existing additives,the multi-cyano,amine-based polybutadiene(AEHTPB-CN)was prepared based on AEHTPB... To simplify the composite propellant formulation and address the current issue of the single-functionality present in existing additives,the multi-cyano,amine-based polybutadiene(AEHTPB-CN)was prepared based on AEHTPB by adopting appropriate synthesis strategies.By replacing 10% of HTPB binder in the propellant formulation,it can effectively enhance the interfacial bond strength between the propellant binder matrix and solid fillers(AP(ammonium perchlorate)and RDX(cyclotrimethylene-trinitramine)),the mechanical properties of the HTPB/AP/RDX/Al propellant were superior to blank control propellant with an improvement of 35.4% in tensile strength,62.0% enhancement in elongation at break,and reduce the propellant burn rate by 10.7% with any energy loss.The function mechanism of AEHTPB-CN was systematically elucidated through experiments and computer simulation techniques.The results show that the tertiary amine group in AEHTPB-CN can react with AP to form ammonium ionic bonds,and the hydroxyl and cyano groups can form hydrogen bonding interactions with AP,which enables AEHTPB-CN to be firmly adsorbed on the AP surface through chemical and physical interactions.For RDX,the interfacial bonding effect of AEHTPB-CN is attributed to their ability to form C-H···N≡C weak hydrogen bonding interaction between the cyano group and RDX methylene group. 展开更多
关键词 hydroxyl-terminated polybutadiene(htpb) htpb propellant Chemical modification Bonding agent MECHANISM
在线阅读 下载PDF
端羟基聚丁二烯与ε-己内酯新型嵌段共聚物的合成与表征 被引量:12
2
作者 柴春鹏 罗运军 +2 位作者 郭素芳 李国平 陈鹤 《含能材料》 EI CAS CSCD 2008年第3期301-304,共4页
端羟基聚丁二烯液体聚合物(HTPB)是广泛应用于固体火箭推进剂的粘合剂。以HTPB为引发剂,在辛酸亚锡催化下,通过ε-己内酯(ε-CL)开环聚合,对HTPB进行改性,得到聚己内酯-端羟基聚丁二烯-聚己内酯(HTBCP)三嵌段共聚物,提高了HTPB与固体火... 端羟基聚丁二烯液体聚合物(HTPB)是广泛应用于固体火箭推进剂的粘合剂。以HTPB为引发剂,在辛酸亚锡催化下,通过ε-己内酯(ε-CL)开环聚合,对HTPB进行改性,得到聚己内酯-端羟基聚丁二烯-聚己内酯(HTBCP)三嵌段共聚物,提高了HTPB与固体火箭推进剂其它组分的相容性。采用凝胶渗透色谱(GPC)、傅立叶红外光谱(FTIR)、核磁共振氢谱(1HNMR)、热失重分析(TG)、差示扫描量热分析(DSC)等表征了共聚物的结构和热性能。结果表明:通过调整HTPB与ε-CL的比例可以控制聚合物的分子量;所有共聚物均有较好的热稳定性,5%的热失重温度高于270℃,且随聚己内酯(PCL)链段含量的增加,共聚物的热稳定性提高。 展开更多
关键词 高分子材料 端羟基聚丁二烯(htpb) 已内酯 开环聚合 嵌段共聚
在线阅读 下载PDF
上一页 1 下一页 到第
使用帮助 返回顶部