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MAPO·HAc衍生物对高燃速IPDI丁羟推进剂低温力学性能的影响
引用本文:刘学,鲁国林.MAPO·HAc衍生物对高燃速IPDI丁羟推进剂低温力学性能的影响[J].固体火箭技术,2002,25(3):45-47.
作者姓名:刘学  鲁国林
作者单位:中国航天科技集团公司四院四十二所,湖北,襄樊,441003
基金项目:国防预研基金项目,项目编号No .12 .6.3 .4。
摘    要:合成了一系列MAPO与HAc(乙酸 )比值不同的MH1~ 5,并考察了其对IPDI固化的高燃速丁羟推进剂低温力学性能的影响 ,研究发现MH对推进剂低温力学性能的影响和MAPO与HAc之比有关 ,初步认为MH对IPDI固化的高燃速丁羟推进剂低温力学性能没有明显改善作用。

关 键 词:丁羟推进剂  力学性能  键合剂  高燃速
文章编号:1006-2793(2002)03-0045-03
修稿时间:2001年7月1日

Effects of derivative of MAPO and HAc on low temperature mechanical property of high burning-rate HTPB IPDI propellant
LIU Xue,LU Guo-lin//The nd Institute of the Fourth Academy of CASC,Xiangfan ,China..Effects of derivative of MAPO and HAc on low temperature mechanical property of high burning-rate HTPB IPDI propellant[J].Journal of Solid Rocket Technology,2002,25(3):45-47.
Authors:LIU Xue  LU Guo-lin//The nd Institute of the Fourth Academy of CASC  Xiangfan  China
Institution:LIU Xue,LU Guo-lin//The 42nd Institute of the Fourth Academy of CASC,Xiangfan 441003,China.
Abstract:A series of MH derivatives with different MAPO/HAc (ethylic acid) ratio were synthesized and the effects of them on the low temperature mechanical property of high burning rate HTPB/IPDI solid propellant were studied. The results show that the effects of MH on the low temperature mechanical property of the propellant depend on with the ratio of MAPO and HAc. The addition of MH can't improve the low temperature mechanical property of high burning-rate HTPB IPDI propellant.
Keywords:hydroxyl terminated polybutadiene propellant  mechanical property  bonding agent  high burning rate
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