| 导弹加速寿命试验方法研究 |
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| 引用本文： | 陈海建,徐廷学,李波,魏勇.导弹加速寿命试验方法研究[J].装备环境工程,2010,7(5):115-118. |
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| 作者姓名： | 陈海建 徐廷学 李波 魏勇 |
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| 作者单位： | 1. 海军航空工程学院,山东,烟台,264001
2. 军事交通运输研究所,天津,300161 |
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| 摘 要： | 寿命试验是确定导弹寿命的重要手段。针对导弹常规寿命存在试验困难、寿命评定不准确的情况,提出了导弹在环境应力影响下的加速寿命试验设计思想,并结合某型导弹自动驾驶仪的实例,设计了加速寿命试验,为今后开展加速寿命试验以估计导弹寿命提供了一种思路。
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| 关 键 词： | 加速寿命 环境应力 导弹 |
Research on Method of Missile Accelerated Life Test |
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| CHEN Hai-jian,XU Ting-xue,LI Bo,WEI Yong.Research on Method of Missile Accelerated Life Test[J].Equipment Environmental Engineering,2010,7(5):115-118. |
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| Authors: | CHEN Hai-jian XU Ting-xue LI Bo WEI Yong |
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| Institution: | 1.Naval Aeronautical and Astronautical University,Yantai 264001,China;2.Institute of Military Transportation,Tianjin 300161,China) |
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| Abstract: | Life prediction is an important means to ensure missile life.The actual service life of missile is difficult to evaluate.By way of analysis and examining,the missile accelerated life test design thought under environmental stress influence was put forward.Combined the living example of certain missile autopilot,accelerated test was designed.The purpose was to provide a way of thinking for accelerated life test to evaluated service life of missile. |
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| Keywords: | accelerated life test environmental stress missile |
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