| 固体推进剂燃速密闭爆发器测试方法 |
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| 引用本文： | 李兆忠,李葆萱.固体推进剂燃速密闭爆发器测试方法[J].固体火箭技术,1993(1):81-86. |
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| 作者姓名： | 李兆忠 李葆萱 |
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| 作者单位： | 西北工业大学 西安710072 |
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| 摘 要： | 介绍了固体推进剂燃速特性的密闭爆发器测试法,给出了该法的物理模型和数学模型,以及用改性双基推进剂试样进行的测试。试验结果表明该方法的测试误差小于2%,有很好的重现性。
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| 关 键 词： | 固体推进剂 燃烧速度 测试技术 |
Solid Propellant Burning Rate Characteristics Measurement in a Closed Bomb |
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| Li Zhaozhong,Li Baoxuan Northwestern Polytechical Universitg,Xi'an.Solid Propellant Burning Rate Characteristics Measurement in a Closed Bomb[J].Journal of Solid Rocket Technology,1993(1):81-86. |
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| Authors: | Li Zhaozhong Li Baoxuan Northwestern Polytechical Universitg Xi'an |
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| Institution: | Li Zhaozhong,Li Baoxuan Northwestern Polytechical Universitg,Xi'an,710072 |
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| Abstract: | The physical model and mathematical model of solid propellant burning rate characteristics measurement in a closed bomb are introduced in this paper,MDB propellant is employed in the experiments.The results show that the error of this method less than 2%(parallel error)and the repeatability are well. |
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| Keywords: | Solid rocket propellant Burning rate Measuring technique Sealed bomb |
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