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固体火箭发动机排气羽流对红外制导信号衰减的计算方法
引用本文:张硕,王宁飞,张平. 固体火箭发动机排气羽流对红外制导信号衰减的计算方法[J]. 固体火箭技术, 2007, 30(5): 408-411
作者姓名:张硕  王宁飞  张平
作者单位:北京理工大学机电工程学院,北京,100081
摘    要:固体火箭发动机排气羽流对红外制导信号的衰减研究,对红外信号的探测与制导具有重要的理论和应用价值。文中主要介绍了红外制导信号的衰减机理,提出了计算排气羽流红外制导信号衰减的有效方法,编制了计算软件DROP,用该软件计算了水雾及颗粒群的光谱透射比,并与SIRRM软件的计算数据进行了对比。结果表明,两者数据基本一致,在工程应用中具有较大的参考价值。

关 键 词:固体火箭发动机  排气羽流  红外衰减  光谱透射比  吸收系数
文章编号:1006-2793(2007)05-0408-04
收稿时间:2006-10-11
修稿时间:2006-12-11

Calculation method on infrared signal attenuation caused by exhaust plume of solid rocket motor
ZHANG Shuo,WANG Ning-fei,ZHANG Ping. Calculation method on infrared signal attenuation caused by exhaust plume of solid rocket motor[J]. Journal of Solid Rocket Technology, 2007, 30(5): 408-411
Authors:ZHANG Shuo  WANG Ning-fei  ZHANG Ping
Affiliation:School of Electro-Mechanical Engineering, Beijing Institute of Technology, Beijing 100081, China
Abstract:The research on infrared signal attenuation caused by solid motor exhaust plume is very important to detection and guidance of infrared signal.The attenuation mechanism of IR signal was mainly introduced,and the effective method for calculating infrared signal attenuation was put forward,then DROP software was programmed.The ratio of spectrum transmission of water drop and solid particle cluster was calculated by means of the DROP software,and the results were compared with calculation data of SIRRM software.The results show that two kinds of data are consistent,which can provide reference to engineering application.
Keywords:solid rocket motor  exhaust plume  infrared attenuation  spectrum transmission ratio  absorption coefficient
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