| 非自燃推进剂固液火箭发动机点火特性试验研究 |
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| 引用本文： | 任国周,浦尔权.非自燃推进剂固液火箭发动机点火特性试验研究[J].固体火箭技术,1997,20(2):27-30. |
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| 作者姓名： | 任国周 浦尔权 |
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| 作者单位： | 中国航天工业总公司三十一所!北京，100074 |
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| 摘 要： | 叙述了非自燃推进剂固液火箭发动机的点火特性，并分析了点火起动程序设计、烟火剂点火器和复合固体引燃器的试验过程，结果表明；应用烟火剂点火器和预设固体引燃器，不仅能保证点火起动安全无误，而且还适用于多种非自燃固液发动机的点火 。
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| 关 键 词： | 固液混合火箭 火箭发动机 点火器 点火试验 |
Experimental Investigation on Ignition Characteristics of Non-Spontaneous Combustion Propellant Hybrid Rocket Motors |
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| Ren Guozhou, Pu Erquan, Li Haijin.Experimental Investigation on Ignition Characteristics of Non-Spontaneous Combustion Propellant Hybrid Rocket Motors[J].Journal of Solid Rocket Technology,1997,20(2):27-30. |
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| Authors: | Ren Guozhou Pu Erquan Li Haijin |
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| Abstract: | The ignition characteristics of non-spontaneous combustion propellant hybrid rocket motors are described . The design of ignition process and tests of pyrotechnic igniters and composite solid propellant boostercharge are discussed . The results show that ignition process are safe and reliable by using pyrotechnic ignitors and composite solid propellant booster charge which can also be applied in the ignition of various nonspontancous combustion propellant hybrid rocket motors. |
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| Keywords: | Hybrid rocket Rocket ignitor Ignition test |
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