摘要
针对机载固体导弹工作时有固体物喷出影响载机安全的问题,采取理论分析和工程实践有机结合的方法,通过试验查证,确定喷出物形态和故障机理,并在结构设计上采取改进措施,解决了喷出物问题,为以后同类型产品类似问题的解决提供了借鉴和参考。
For the airborne security problems which affected by some missile solid ejecta during working period, and taking the method of combining the theoretical analysis and engineering practice together, and through the testing verification, the ejectas modality and the failure mechanism were ensured. At the same time, improving the structural design was improved to deal with the problem of ejecta. Its good effected was reference for solving the similar problems of this type products.
出处
《海军航空工程学院学报》
2010年第6期675-678,共4页
Journal of Naval Aeronautical and Astronautical University
关键词
导弹
喷出物
载机安全
missile
ejecta
airborne security