火炸药学报Issue(3)：9-14,21,7.DOI:10.14077/j.issn.1007-7812.2015.03.002
固体推进剂燃速测试技术研究进展
Research Progress in the Burning Rate Measurement Technology of Solid Propellant
摘要
Abstract
The current research situation of static burning rate,dynamic burning rate and measurement technology of burning rate under specific environment for solid propellant,and characteristics of various burning rate measure-ment methods were reviewed.Considering that the general development rule of solid propellant burning rate meas-urement technology is that from the static burning rate measurement gradually developed into the dynamic burning rate measurement.On the basis of the dynamic burning rate measurement,the rotating overload burning rate meas-urement technology and burning rate measurement technology under the transient pressure condition appeared.The existing burning rate measurement technology is also used to test the combustion performance of commonly used high-energy additives in solid propellant.The future development direction of the combustion performance testing technology of solid propellant,including high pressure (ultra pressure)combustion performance measurement tech-nology,ultra low pressure (vacuum,)combustion performance measurement technology and low temperature micro-gravity combustion performance measurement technology etc,is pointed out with 55 references.关键词
物理化学/固体推进剂/静态燃速/动态燃速/燃速测试Key words
physical chemistry/solid propellant/static burning rate/dynamic burning rate/burning rate measurement分类
军事科技引用本文复制引用
裴庆,赵凤起,罗阳,徐司雨..固体推进剂燃速测试技术研究进展[J].火炸药学报,2015,(3):9-14,21,7.基金项目
国家自然科学基金资助 （）
