Are All Solid Propellant Burning Rate Modifiers Catalysts?

被引:13
作者
Kalman, Joseph [1 ]
机构
[1] Calif State Univ Long Beach, Dept Mech & Aerosp Engn, 1250 Bellflower Blvd, Long Beach, CA 90840 USA
关键词
ammonium perchlorate; burning rate; solid propellant; catalysis; modifier;
D O I
10.1002/prep.202200148
中图分类号
O69 [应用化学];
学科分类号
081704 ;
摘要
Solid rocket motors are used for both national defense and launch vehicles. The internal ballistics of the motor depend on the propellant burning rate, which is often modified by burning rate enhancers. Despite the common use, there is not a complete mechanistic understanding of how these modifiers influence the combustion process. In this comment, it is argued that these additives can influence propellant combustion as a catalyst, via thermodynamic means, or a combination. An approach is suggested on how to classify traditional and novel burning rate modifiers as a first step to improving the scientific community's knowledge on the matter.
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页数:4
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