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高压燃速声发射测试技术研究
引用本文:徐再荣.高压燃速声发射测试技术研究[J].固体火箭技术,1997(3).
作者姓名:徐再荣
作者单位:中国航天工业总公司四院7416厂!西安,710000
摘    要:简要介绍了一种高压燃速声发射测试方法的原理、测试系统及其技术参数。在3~20MPa下进行了不同燃速的测定,结果表明,该系统测试相对误差小于0.9%.

关 键 词:固体推进剂  声发射  燃速  测试技术

Study on the High-pressure Bunring Rate Acoustic Emission Measuring
Xu Zairong.Study on the High-pressure Bunring Rate Acoustic Emission Measuring[J].Journal of Solid Rocket Technology,1997(3).
Authors:Xu Zairong
Abstract:The principle of a high-pressure burning rate measuring method, measuring system and its main technical parameters are briefly presented. It is used for measuring of the burning rates at 3~20MPa. The measured results show that the relative error of the measuring system is less than 0. 9%.
Keywords:Solid propellant Acoustic emission Burning rate Measuring technique  
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