Influence of humidity on the heat decomposition speed of single-base propellant

被引:0
|
作者
Zhang Renhe
Lu Guie
Liu Kunlun
Deng Tao
Deng Hanbo
机构
关键词
single-base propellant; adiabatic decomposition; relative humidity; Accelerating Rate Calorimetry;
D O I
暂无
中图分类号
V [航空、航天];
学科分类号
08 ; 0825 ;
摘要
The thermal process measurement experiment of single-base propellant were determinated using Accelerating Rate Calorimetry in the different humidity. The experimental result was discussed and analysed. Find that the shape of experiment sample has the definitive influence on the heat decomposition characteristic measure of single-base propellant. Along with the increment of the degree of humidity, the temperature which propellant begins decomposing gradually becomes shorter, but after the humidity surpasses 84%, the temperature gets higher to some extent, and is lower than which the humidity is 2% although the humidity gets to 92%.
引用
收藏
页码:206 / 209
页数:4
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