Studying on Burning Rate of Propellant under Diverse Parameters

被引：0
|
作者：
Chu, Hung-Ta [1 ]
机构：
[1] Chung Shan Inst Sci & Technol, POB 90008-21-4, Pingtung 947, Taiwan
来源：
WORLD CONGRESS ON ENGINEERING AND COMPUTER SCIENCE, WCECS 2012, VOL II | 2012年
关键词：
AP; burning rate;
D O I：
暂无
中图分类号：
TP39 [计算机的应用];
学科分类号：
081203 ; 0835 ;
摘要：
An experimental investigation on the burning rates and mechanical properties of HTPB propellants with Fe2O3 and AP is carried out at pressure in the range from 10 to 14 MPa and universal tester. The content of Fe2O3 and the oxidizer particle size distribution have a considerable effect on the burning rate of the propellant.
引用
收藏
页码：749 / 751
页数：3
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