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HTPB/AP推进剂的慢速烤燃特征
引用本文:陈中娥,唐承志,赵孝彬.HTPB/AP推进剂的慢速烤燃特征[J].含能材料,2006,14(2):155-157.
作者姓名:陈中娥  唐承志  赵孝彬
作者单位:航天科技集团公司四院四十二所,湖北,襄樊,441003
摘    要:介绍了弹药慢速烤燃试验方法和评判标准,初步分析了影响弹药慢速烤燃响应的因素。对国外在HTPB/AP推进剂慢速烤燃特性方面的研究进行了述评,研究表明,高氯酸铵热分解形成的多孔性形貌是导致AP基推进剂慢速烤燃响应剧烈的重要因素。在此基础上提出了改善HTPB/AP推进剂慢速烤燃响应的技术途径。

关 键 词:热化学  慢速烤燃  高氯酸铵  HTPB推进剂
文章编号:1006-9941(2006)02-0155-03
收稿时间:2004-11-12
修稿时间:2005-04-03

Characteristics of HTPB/AP Propellants in Slow Cook-off
CHEN Zhong-e,TANG Cheng-zhi and ZHAO Xiao-bin.Characteristics of HTPB/AP Propellants in Slow Cook-off[J].Chinese Journal of Energetic Materials,2006,14(2):155-157.
Authors:CHEN Zhong-e  TANG Cheng-zhi and ZHAO Xiao-bin
Affiliation:The 42rid Institute of the Fourth Academy of CASC, Xiangfan 441003, China
Abstract:The method and assessment standard of munition in slow cook-off test is introduced and the factors affecting slow cook-off response of munition are analyzed.The characteristics of slow cook-off of HTPB/AP propellants at abroad are summarized.Results show the porous materials produced by thermal decomposition of ammonium perchlorate is the important factor causing HTPB/AP propellants to demonstrate violent reactions in slow cook-off test.Furthermore,the techniques to improve the slow cook-off response of AP based propellants are pointed out.
Keywords:thermal chemistry  slow cook-off  ammonium perchlorate  HTPB propellant
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