| Ap复合固体推进剂稳态燃烧模型综述 |
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| 引用本文： | 张炜,朱慧.Ap复合固体推进剂稳态燃烧模型综述[J].固体火箭技术,1994,17(1):38-46. |
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| 作者姓名： | 张炜 朱慧 |
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| 作者单位： | 国防科技大学，国防科技大学 湖南长沙 410073，湖南长沙 410073 |
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| 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。
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| 关 键 词： | 合成推进剂 燃烧性能 燃速 |
A Review of Ap Composite Solid Propellent Steady Combustion Models |
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| Zhang Wei Zhu Hui.A Review of Ap Composite Solid Propellent Steady Combustion Models[J].Journal of Solid Rocket Technology,1994,17(1):38-46. |
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| Authors: | Zhang Wei Zhu Hui |
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| Abstract: | 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. |
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| Keywords: | Composite propellant Propellant combustion Propellant burning rate |
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