| 固体推进剂羽焰红外辐射强度测试技术 |
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| 引用本文： | 张劲民,袁华,刘俊峰.固体推进剂羽焰红外辐射强度测试技术[J].固体火箭技术,2004,27(2):161-164. |
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| 作者姓名： | 张劲民 袁华 刘俊峰 |
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| 作者单位： | 中国航天科技集团公司四院四十二所,襄樊,441003;中国航天科技集团公司四院四十二所,襄樊,441003;中国航天科技集团公司四院四十二所,襄樊,441003 |
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| 摘 要： | 针对低特征信号推进剂研究的需要，研制了羽焰红外辐射测试系统，并进行了几种配方的推进剂羽焰红外辐射强度测试。该系统主要包括探测单元、光路系统、信号处理单元和自校准黑体等，测试精度优于4％，使用性能良好，能准确表征推进剂红外辐射的水平。
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| 关 键 词： | 固体推进剂 羽焰 红外辐射 |
| 文章编号： | 1006-2793(2004)02-0161-04 |
| 修稿时间： | 2004年2月25日 |
IR measuring technology for solid propellant plume |
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| ZHANG Jin-min,YUAN Hua,LIU Jun-fengThe nd Institute of the Fourth Academy of CASC,Xiangfan,China..IR measuring technology for solid propellant plume[J].Journal of Solid Rocket Technology,2004,27(2):161-164. |
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| Authors: | ZHANG Jin-min YUAN Hua LIU Jun-fengThe nd Institute of the Fourth Academy of CASC Xiangfan China |
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| Institution: | ZHANG Jin-min,YUAN Hua,LIU Jun-fengThe 42nd Institute of the Fourth Academy of CASC,Xiangfan441003,China. |
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| Abstract: | IR measuring system was developed aiming at the demand of low characteristic signal propellants. The system was used for measuring several formula propellant plumes.This system mainly consists of dectection unit,light-circuit system,signal treatment unit,and self-calibrated black bady,etc., with the measuring accuracy higher than 4%,and good operational property, the system can be used to accurately characterize IR measuring level of solid propellant plume. |
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| Keywords: | solid propellant plume infrared radiation |
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