Ap复合固体推进剂稳态燃烧模型综述  

A Review of Ap Composite Solid Propellent Steady Combustion Models

作　　者：张炜[1] 朱慧[1] 

机构地区：[1]国防科技大学,湖南长沙410073

出　　处：《固体火箭技术》1994年第1期38-46,共9页Journal of Solid Rocket Technology

摘　　要：对目前国内外典型的且较为成熟的高氯酸铵复合固体推进剂稳态燃烧模型进行了简要的综述,涉及的燃烧模型有:GDF模型、HR模型、BDP模型、临界粒径模型、PEM模型、CIT/JPL模型、两区模型和价电子模型。对上述模型的适用范围、特点和优缺点进行了较为客观的评价。The classic and ripe steady combustion models of Ap composite solid propellant both in China and abroad are reviewed. The combustion models introduced were GDF Model, HR Model, BDP Model, Critical Diameter Model, PEM, CIT/JPL Model, Two Region Model and Valent Electron Model. The applicable region, characteristics, strong and weak points of the models are also evaluated objectively.

关 键 词：合成推进剂 燃烧性能 燃速 

分 类 号：V512.3[航空宇航科学与技术—航空宇航推进理论与工程]