Effect of nitramine on energy and burning rate of low burning rate HTPB propellant

被引：0
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作者：
Lu, G. [1 ]
机构：
[1] The 42nd Inst. of the Fourth Acad., CASC, Xiangfan 441003, China
来源：
Guti Huojian Jishu/Journal of Solid Rocket Technology | 2001年 / 24卷 / 02期
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摘要：
An application investigation of the nitramine (RDX,HMX) to the low burning rate HTPB propellants was carried out in the view of energetic property and combustion performance. The results show that the partial substitution of nitramine for ammonium perchlorate can raise theoretical specific impulse and reduce pressure exponent of propellants greatly, while the effect on burning rate is very minor.
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页码：45 / 47
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