| 燃气参数及材料缺陷对绝热层烧蚀率影响的试验研究 |
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| 引用本文： | 黄祖荫,何国强.燃气参数及材料缺陷对绝热层烧蚀率影响的试验研究[J].固体火箭技术,1995,18(2):70-76. |
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| 作者姓名： | 黄祖荫 何国强 |
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| 作者单位： | 西安四院四十一所，西北工业大学 |
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| 摘 要： | 提出了固体火箭发动机绝热层烧蚀性能的试验评估方法，建立了在不同燃气参数和绝热层材料有缺陷条件下的烧蚀模型及烧蚀率经验公式，并对绝热层烧蚀率影响程度进行了分析，为绝热层设计提供了依据。
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| 关 键 词： | 固体推进剂 火箭发动机 隔热材料 烧蚀试验 |
Experimental Investigation of the Effects of Combustion Gas and Material Defects on the Insulation Ablation Rate |
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| Huans Zuyin.Experimental Investigation of the Effects of Combustion Gas and Material Defects on the Insulation Ablation Rate[J].Journal of Solid Rocket Technology,1995,18(2):70-76. |
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| Authors: | Huans Zuyin |
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| Abstract: | An experimental evaluation method for the insulation ablation in the solid rocket motor was proposed. An insulation model and experimental formula under different gas paramcnters and materials defects are built up and used for analyzing the effects of the insulation ablation rate. It can be taken as a basis of design. |
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| Keywords: | Solid propellant rocket engine Thermal insulating material Ablation test |
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