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在高燃速推进剂中粗颗粒铝粉的作用
杨凤仪
航空航天部806所
摘要:
本文用50μm铝粉作复合固体推进剂金属燃料,与大量超细氧化剂(AP)组成合理级配,改善了药浆流变特性,有利于提高燃速。50μm铝粉的推进剂药条的燃速及φ118发动机推进剂的燃速比相应的填加30μm铝粉的高2~3mm/s。讨论了50μm铝粉对推进剂工艺和燃速所起的作用。
关键词:  固体推进剂  推进剂燃速  流变学  特性
DOI:
分类号:
基金项目:
THE FUNCTION OF COARSE-PARTICLE ALUMINIUM POWDER IN HIGH BURNING RATE SOLID PROPELLANT
Yang FengYi
The 806th Research Institute
Abstract:
The composite solid propellants containing 50μm Al powder as a combustible ingredient are described. An excellent aggregation composed of 50μm Al powder and a large quantity of finer particle size of oxidizer (AP) ameliorats the Theological characteristics of propellant slurry and increases the burning rate. The burning rate of the strand and the propellants in a test motor with φ118 diameter increases by 2-3mm/s with the addition of 50μm Al powder compared with the addition of 30μm. The effects of 50μm Al powder on the burning rate and propellant technology are discussed.
Key words:  Solid propellant  Propellant burning  Rheology  Characteristic