| 郭迅,郭强岭.空空导弹爆炸分离冲击试验分析[J].装备环境工程,2016,13(4):78-82. GUO Xun,GUO Qiang-ling.Pyroshock Test for Air-to-Air Missile[J].Equipment Environmental Engineering,2016,13(4):78-82. |
| 空空导弹爆炸分离冲击试验分析 |
| Pyroshock Test for Air-to-Air Missile |
| 投稿时间：2016-03-19 修订日期：2016-08-15 |
| DOI：10.7643/ issn.1672-9242.2016.04.013 |
| 中文关键词: 空空导弹 爆炸分离冲击 冲击响应谱 |
| 英文关键词:air-to-air missile pyroshock SRS |
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| 中文摘要: |
| 目的 获取某型空空导弹爆炸分离冲击试验的条件及方法。方法 针对爆炸分离冲击环境高频响、高量级、短时间等特性，分析获取爆炸分离冲击信号的方法，以及相应的冲击响应谱、归纳数据处理方法。结果 通过测试得到某型空空导弹的爆炸分离数据，进行了冲击响应谱和归纳分析，得到了不同测点位置爆炸分离冲击的特性。结论 形成了一种适用于空空导弹的合理、易实施的爆炸分离冲击试验条件及试验方法。 |
| 英文摘要: |
| Objective To obtain the conditions and methods of pyroshock test for air-to-air missile. Methods According to the characteristics of pyroshock, such as high frequency, high acceleration and short-time duration, the method to obtain the pyroshock signal as well as the shock response spectrum and inductive data processing method were analyzed. Results Pyroshock data of air-to-air missile were obtained by test. Characteristics of pyroshock at different measuring points were acquired through shock response spectrum (SRS) and statistical induction. Conclusion Testing conditions and methods of a reasonable and implementary pyroshock test for air-to-air missile are given. |
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