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

页码：253 / 255

页数：3