Emission imaging of AP/HTPB propellant sandwich combustion

被引:20
作者
Chorpening, BT [1 ]
Brewster, MQ
机构
[1] Natl Energy Technol Lab, Morgantown, WV USA
[2] Dept Mech & Ind Engn, Urbana, IL USA
关键词
solid propellant rockets; laminar diffusion flames;
D O I
10.1080/713713012
中图分类号
O414.1 [热力学];
学科分类号
摘要
Ultraviolet emission imaging (305-315 nm) was used to study the combustion of sandwiches of ammonium perchlorate (AP) and hydroxyl-terminated polybutadiene (HTPB) in nitrogen at pressures up to 32 atm. with binder layers from 50 to 450 mum in thickness. The emission imaging was combined with a novel backlighting technique to allow determination of the corresponding surface shape during combustion, The results indicated that the interface regression rate of IPDI-cured samples undergoing laser-assisted deflagration (120 W/cm(2) average flux) is nearly independent of the binder thickness for binders thicker than 100 pm. The pressure exponent of the regression rate is 0,31 up to 15 atm, then increases with pressure from 15 to 32 atm. Two primary flame regimes were identified: a regime of high Peclet and Damkohler numbers which exhibits a split base in the ultraviolet flame emission, and a regime of low Peclet and Damkohler numbers which exhibits a merged flame base, A third. "lifted" flame region, in which the strongest flame emission starts several hundred microns above the solid surface, occurs with low Damkohler numbers and high Peclet numbers, The effects of Pe and binder oxygenation (by fine-AP) on the size of the diffusion flame and the
引用
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页码:39 / 60
页数:22
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