| 航天火工品输出性能试验及其作用裕度的确定 |
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| 引用本文： | 王凯民,符绿化.航天火工品输出性能试验及其作用裕度的确定[J].火工品,1999(3):51-56. |
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| 作者姓名： | 王凯民 符绿化 |
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| 作者单位： | 1. 北京理工大学,北京,100081
2. 中国兵器工业第213研究所,陕西,西安,710061 |
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| 摘 要： | 对航天器用输出作功的火工品，按类别（驱动系统、点火装置、导爆索装置）介绍了其输出性能试验和作用裕度的确定方法，简述了各种试验方法的应用及其特点。
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| 关 键 词： | 火工品 输出性能试验 作用裕度 |
| 文章编号： | 1003-1480(1999)03-0051-06 |
| 修稿时间： | 1998-12-16 |
Output Performance Test and Functional Margin Determination of Initiating Explosive Device in Aerospace System |
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| WANG Kai-min,FU Lu-hua.Output Performance Test and Functional Margin Determination of Initiating Explosive Device in Aerospace System[J].Initiators & Pyrotechnics,1999(3):51-56. |
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| Authors: | WANG Kai-min FU Lu-hua |
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| Abstract: | For the initiating explosive device in the aerospace system, output performance test and functional margin of determination are introduced according to its classification such as driving system, ignition device and detonating cord device. The application and characteristics of the test methods are briefly described. |
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| Keywords: | Initiating explosive device Output perfomance test Functional margin |
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