会议专题

Combustion Characteristics of Solid Propellant Under Laser Irradiation

This paper studies combustion characteristics under laser irradiation of three groups of propellants. Our original fuel-rich propellants (AP/HTPB=20/80) are non-self-combustible propellant at back pressure up to 1.0 Mpa, laser could control including, ignition, interruption and re-ignition easily, however, SQ-2 and HTPB propellant are self-sustained combustion propelllant, without laser irradiation they can burn continuously. The dependence of burning rate on laser power density of SQ-2 and HTPB propellant could be described by a piece-wise function. The break point is an important character of these solid propellants, one of main reason induced break point is the loss of radiant energy before the radiant energy reaches the surface of condensed phase.

QIN Zhao SHEN Ruiqi DU Jiangyuan WU Lizhi ZHANG Wei YE Yinghua HU Yan ZHU Peng

School of Chemical Engineering, Nanjing University of Science and Technology, Nanjing 210094, China

国际会议

2011 International Autumn Seminar on Propellants,Explosives and Pyrotechnics(2011国际推进剂、炸药、烟火技术秋季研讨会)

南京

英文

731-735

2011-09-20(万方平台首次上网日期,不代表论文的发表时间)