Enhanced propellant combustion with nanoparticles

被引：174
|
作者：
Armstrong, RW [1 ]
Baschung, B
Booth, DW
Samirant, M
机构：
[1] AFRL, MNME, Eglin AFB, FL 32542 USA
[2] ISL, French German Res Inst St Louis, F-68301 St Louis, France
[3] LLC, Irvine, CA 92606 USA
来源：
NANO LETTERS | 2003年 / 3卷 / 02期
关键词：
D O I：
10.1021/nl025905k
中图分类号：
O6 [化学];
学科分类号：
0703 ;
摘要：
Enhanced burn rate results are presented for ammonium perchlorate/Al nanoparticle strand burners at atmospheric (and higher) pressure and for the comparative combustion in a high pressure closed vessel of a solid propellant containing 15% of either conventional micrometer-scale Al or nanometric Al. The burn rate at the smallest nanometric Al particle size appears to be asymptotically approaching an inverse particle-diameter-squared dependence.
引用
收藏
页码：253 / 255
页数：3
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