固体火箭技术2017，Vol.40Issue(6)：720-724,5.DOI:10.7673/j.issn.1006-2793.2017.06.008
固体组分含量对GAP/CL-20推进剂燃烧性能的影响
Effect of content of solid components on combustion performance of GAP/CL-20 propellant
周晓杨 1唐根 1庞爱民 1吴芳 1宋会彬 1徐海元 1王艳萍 1徐星星 1周水平1
作者信息
- 1. 湖北航天化学技术研究所,襄阳 441003
- 折叠
摘要
Abstract
The effect of main formation factors,such as the solid content,the relative content of AP/CL-20,CL-20/Al,Al/AP on the combustion performance of GAP/CL-20 high-energy solid propellant was studied by the determination of burning rate and the calculation of the pressure exponent.The results show that the burning rate and the pressure exponent all increase when the solid content increases within a certain range.Increasing the relative content of AP from AP/CL-20 and CL-20 from CL-20/Al make the burning rate increase,while the pressure exponent decrease.The increase of the relative content of Al from Al/AP lead the burning rate to decrease,while the pressure exponent increase.The influence mechanism was also analyzed.关键词
高能固体推进剂/固含量/相对含量/燃速/燃速压强指数Key words
high-energy solid propellant/solid content/relative content/burning rate/pressure exponent分类
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周晓杨,唐根,庞爱民,吴芳,宋会彬,徐海元,王艳萍,徐星星,周水平..固体组分含量对GAP/CL-20推进剂燃烧性能的影响[J].固体火箭技术,2017,40(6):720-724,5.
