导弹
交货地点
休克(循环)
振动
航空学
结构工程
工程类
航空航天工程
计算机科学
法律工程学
物理
声学
医学
农学
生物
内科学
作者
Man-Dal Kim,Seong-Wook Hong,Jong Hoon Hyun,Dong‐Kook Kim,Seungjun Lee
出处
期刊:한국생산제조시스템학회지
[The Korean Society of Manufacturing Technology Engineers]
日期:2015-06-15
卷期号:24 (3): 342-347
被引量:1
标识
DOI:10.7735/ksmte.2015.24.3.342
摘要
Article history: The launcher pod for missiles capable of carrying a range of different warheads has been designed to be mounted on the tracked vehicle of the hybrid weapon system (HWS). In the development of this launcher pod, its structure was designed to be resilient to damage caused by shock and vibration, as well as preventing assembly errors due to the spring-back of the main composite cover and interfacing parts. This study investigated the design of the newly developed launcher pod, with its hybrid composite–metal structure, through simulation and experiment. Both simulation and actual experiments showed that the structure of the launcher is resilient to vibration and shock. The launcher pod was also subjected to vibration and shock tests to verify its performance.
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