给出了对这些型号挂弹钩的计算实例，讨论了各种结构参数和物理参数对弹射性能的影响规律。
Several simulation examples are given, and the effect of different parameter structure on ejecting device is discussed.
通过调查飞机挂弹架次比例，发现情况变化随意性很强，基本无统计规律可循，因而按每架次实际起飞外挂重量计算疲劳损伤显得尤为必要。
The investigation shows that actual take-off suspension weights chang considerably and irregularly, so it is important to calculate fatigue damage based on actual suspension weights for each flight.
第五，简要地叙述了弹载导航计算机的软硬件设计、主控软件的流程以及第一次原理样弹挂飞与投掷试验。
Fifthly, it is introduced that the software, hardware design of the guidance computer, the flow chart of control software and the first throw experimentation.
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