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密闭燃烧器在固体火箭推进剂燃速测定中的应用研究
引用本文:李葆萱,肖育民.密闭燃烧器在固体火箭推进剂燃速测定中的应用研究[J].弹箭技术,1997,9(1):9-14.
作者姓名:李葆萱  肖育民
作者单位:西北工业大学
摘    要:密闭燃烧器法是一种能测定很宽压强范围内固体火箭推进剂速特性及变化情况的快速测量方法。本文阐述了该方法的基本原理,实验研究。介绍实验曲线处理与数值分析,并提出了一种复合推进剂的一种双基推进剂测试结果。

关 键 词:固体推进剂  燃烧器  燃速  测定

Application of closed burner for measuring burning rate of solid rocket propellant
Authors:Li Baoxuan  Xiao Yumin  Li Fengchun  He Guoqiang  Liu Huaqiang
Abstract:Burning rate measurement with closed burner is a rapid method for measuring burning rate character and its change of solid rocket propellants in a wide pressure range. In this paper the authors deserible the fundamentals and experimental research of this method. The processing on expermental curve and data analysis are also introduced. At the end of this paper some test results are given about a double-based propenllant and a composition propoellant.
Keywords:Closed burner  Burning rate character    
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