Propellant formulation factors and metal agglomeration in combustion of aluminized solid rocket propellant

被引：100

作者：

Babuk, VA ^{[1
]}

Vassiliev, VA ^{[1
]}

Sviridov, VV ^{[1
]}

机构：

[1] Balt State Tech Univ, St Petersburg, Russia

来源：

COMBUSTION SCIENCE AND TECHNOLOGY | 2001年 / 163卷 / 1-6期

关键词：

composite solid propellant; combustion; agglomeration; ammonium perchlorate; ammonium dinitramide;

D O I：

10.1080/00102200108952159

中图分类号：

O414.1 [热力学];

学科分类号：

摘要：

An experimental study of aluminized solid rocket propellant combustion was conducted in order to determine the influence of various propellant formulation factors on metal agglomeration, The results allowed us to determine the dependencies of the agglomeration process characteristics on the physical and mechanical properties of the propellant binder, the particle size of the metal fuel, the type of film covering the original metal particles, and the type of oxidizer in the propellant. These results, combined with earlier data, were used to develop a physical picture of the agglomeration process, which may serve as the basis for conducting analysis of the influence of various propellant formulation factors on agglomeration.

引用

页码：261 / 289

页数：29