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

共 50 条

[41] Flame stabilization in cryogenic propellant combustion
Herding, G
Snyder, R
Scouflaire, P
Rolon, C
Candel, S
TWENTY-SIXTH SYMPOSIUM (INTERNATIONAL) ON COMBUSTION, VOLS 1 AND 2, 1996, : 2041 - 2047
[42] NONACOUSTIC INSTABILITY OF COMPOSITE PROPELLANT COMBUSTION
BECKSTEAD, MW
RYAN, NW
BAER, AD
AIAA JOURNAL, 1966, 4 (09) : 1622 - +
[43] STABILITY OF SOLID-PROPELLANT COMBUSTION
BYCHKOV, VV
LIBERMAN, MA
PHYSICAL REVIEW LETTERS, 1994, 73 (14) : 1998 - 2000
[44] Progress on combustion catalysts of solid propellant
Wei, Zhi-Xian (zx_wei@126.com), 2015, Institute of Chemical Materials, China Academy of Engineering Physics (23):
[45] Propellant formulation factors and metal agglomeration in combustion of aluminized solid rocket propellant
Babuk, VA
Vassiliev, VA
Sviridov, VV
COMBUSTION SCIENCE AND TECHNOLOGY, 2001, 163 (1-6) : 261 - 289
[46] HYDRODYNAMIC STABILITY OF SOLID AND LIQUID PROPELLANT COMBUSTION
BECHTOLD, JK
MARGOLIS, SB
COMBUSTION SCIENCE AND TECHNOLOGY, 1989, 68 (1-3) : 49 - 84
[47] MODEL FOR DOUBLE-BASE PROPELLANT COMBUSTION
BECKSTEAD, MW
AIAA JOURNAL, 1980, 18 (08) : 980 - 985
[48] LAWS OF COMBUSTION OF A SOLID-PROPELLANT SANDWICH
ERMOLAEV, BS
KOROTKOV, AI
FROLOV, YV
COMBUSTION EXPLOSION AND SHOCK WAVES, 1973, 6 (03) : 251 - 257
[49] Computational models of combustion of nonmetallized heterogeneous propellant
Surzhikov, ST
Krier, H
HIGH TEMPERATURE, 2003, 41 (01) : 95 - 128
[50] Study of combustion characteristics of RDX/HTPB propellant
Tu, Yongzhen
Wang, Chaozhen
Guti Huojian Jishu/Journal of Solid Rocket Technology, 1995, 18 (02):

← 1 2 3 4 5 →