含能材料2011，Vol.19Issue(1)：74-77,4.DOI:10.3969/j.issn.1006-9941.2011.01.017
发射药的火焰燃烧温度计算与测定分析
Calculation and Measurement Analysis of Propellant Burning Temperature
廖静林 1江劲勇 1路桂娥 1常文平 1翟宏昌2
作者信息
- 1. 军械工程学院军械技术研究所,河北,石家庄,050003
- 2. 75407部队,广东,湛江,524100
- 折叠
摘要
Abstract
The burning temperature of single-based (H100 and H130 ) ,SF (SF-3) ,modified double-based propellants (171-25 and GT) were calculated and measured at constant pressure.The difference between adiabatic flame temperature approximation calculation result and measured result was compared.The calculation results are consistent with experimental results,the maximum flame temperatures of H130 and SF-3 propellant are 2215 K,2230 K.As the candidate of hot source,the double-based propellant is better than the single-based propellant.The colorimetric temperature measurement can not reflect the accurate temperature of modified double-based propellants.关键词
物理化学/发射药/比色测温/火焰燃烧温度Key words
physical chemistry/ propellant/ colorimetric temperature measurement/ combustion temperature分类
军事科技引用本文复制引用
廖静林,江劲勇,路桂娥,常文平,翟宏昌..发射药的火焰燃烧温度计算与测定分析[J].含能材料,2011,19(1):74-77,4.
