This article introduces a designing means of mold of the fibre winding solid rocket motor combustion chamber shell.
介绍一种固体火箭发动机燃烧室壳体纤维缠绕芯模的设计。
As an example, the strength of a solid fuel rocket engine shell is calculated.
作为一个例子，计算了一个固体火箭发动机壳体的强度。
GA to resolve process route optimization of solid rocket motor shell is studied.
研究了基于遗传算法的固体发动机壳体工艺流程面向成本优化问题。
The calculation using different atmosphere data shows that the range of long-range shell-rocket is affected obviously by different standard atmospheres.
计算结果表明，高空条件下不同标准大气对远程弹箭射程的影响很大。
The calculation using different atmosphere data shows that the range of long-range shell-rocket is affected obviously by different standard atmospheres.
计算结果表明，高空条件下不同标准大气对远程弹箭射程的影响很大。
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