Synthesis of multifunctional additives for solid propellants: Structure,properties and mechanism

被引:0
|
作者
Pingan Zhang [1 ]
Lina Sun [2 ]
Jianmin Yuan [3 ]
Jianru Deng [1 ]
机构
[1] College of Chemistry and Chemical Engineering, Hunan University
[2] Hu Bei Sanjiang Aerospace Jianghe Chemical Technology Co., Ltd
[3] College of Material Science and Engineering, Hunan University
关键词
D O I
暂无
中图分类号
V512 [固体推进剂];
学科分类号
080502 ;
摘要
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.
引用
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页码:308 / 316
页数:9
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