首页 | 本学科首页   官方微博 | 高级检索  
     检索      

降低丁羟推进剂高压压强指数研究
引用本文:徐馨才,吴祝骏.降低丁羟推进剂高压压强指数研究[J].推进技术,1993,14(6):73-76.
作者姓名:徐馨才  吴祝骏
作者单位:航空航天部806所 (徐馨才),航空航天部806所(吴祝骏)
摘    要:研究了某些化合物对丁羟(HTPB)复合固体推进剂燃速压强指数的影响。实验发现,FG是一种降低HTPB推进剂压强指数的高效添加剂。当FG与亚铬酸铜组合使用时,可在提高推进剂燃速的同时大幅度地降低燃速压强指数。文中对FG的作用机理作了初步探讨。

关 键 词:端羟基  聚丁二烯  推进剂  燃烧速度

RESEARCH ON LOWERING THE PRESSURE EXPONENT OF HTPB PROPELLANT AT HIGH PRESSURE
Xu Xingcai and Wu Zhujun.RESEARCH ON LOWERING THE PRESSURE EXPONENT OF HTPB PROPELLANT AT HIGH PRESSURE[J].Journal of Propulsion Technology,1993,14(6):73-76.
Authors:Xu Xingcai and Wu Zhujun
Institution:The 806th Research Institute
Abstract:In the present paper, an investigation on effects of some compounds on the pressure exponent of HTPB propellant is presented. The experiment indicates that FG is a good additive for reducing the pressure exponents. When FG and YB are incorporated, they may obviously reduce the pressure exponent of HTPB propellant as well as enhancing the burning rate. In the paper, the catalysis mechanism of FG is preliminarily discussed.
Keywords:Hydroxy polybutadiene propellant  Propellant burning rate  Catalyst  
本文献已被 CNKI 维普 等数据库收录!
点击此处可从《推进技术》浏览原始摘要信息
点击此处可从《推进技术》下载免费的PDF全文
设为首页 | 免责声明 | 关于勤云 | 加入收藏

Copyright©北京勤云科技发展有限公司  京ICP备09084417号