test-type launcher

This paper describes the modal analysis test made for the director of a rocket launcher and the modal parameters identified with the mobility circle fitting method useful data are provided for the study of the dynamic properties of the director.

本文对火箭炮定向器作了模态分析试验，用导纳圆拟合法识别了它的模态参数，为研究定向器的动态特性提供了数据。

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Based on the ANSYS analysis software and simulation of the strength test, it was quantitatively proved that increasing the chamfering on the slot root of the rail could obviously reduce the stress concentration and enhance the intensity of the launcher housing.

基于ANSYS分析软件平台以及模拟强度试验对导轨撕裂部位进行强度分析，定量说明了此圆角增大可以明显改善导轨槽处的应力集中，增大某发射装置壳体的强度余量。

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The Static Test Study of Composite Rocket Launcher

复合材料火箭发射器的静态测试研究

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Through test on pigging receiver and launcher enduring pressure, determined is main reason resulting in quick opening closure enduring pressure on pigging system, and resolving method is put forward.

通过对收发球筒进行带压试验，找出导致清管系统快开盲板带压运行的主要原因，并提出解决的措施。

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Design and Realization of General Test System for Certain Launcher Circuit Boards

某发射机构电路板通用检测系统设计与实现

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