直升机载空地导弹挂飞寿命试验技术研究  

Research on Testing Technology for Airborne Air-to-ground Missile Hanging Flight Lifespan

作　　者：刘旭琳 周金林 李玉玲 

机构地区：[1]中国兵器第三研究院,西安710065

出　　处：《环境技术》2017年第4期74-75,79,共3页Environmental Technology

摘　　要：本文主要对直升机载空地导弹挂飞阶段的可靠性指标进行了研究,确定了挂飞寿命考核的试验方法和试验步骤,对不同试验方案进行了对比,开展了整弹的挂飞寿命摸底试验,对直升机载设备的挂飞寿命考核具有借鉴意义。This paper mainly researched the reliability guide lines of airborne air-to-ground missile during the hanging flight process and confirmed the testing methods and procedures for longevity tests Through comparing different experimental schemes, the experiments with the whole air-to-ground missile system are carried out, which is primarily important to the longevity tests.

关 键 词：挂飞寿命 耐久性振动 疲劳公式 

分 类 号：TJ76[兵器科学与技术—武器系统与运用工程]