Both the structure and the use of solid rocketmotorcase skirts are presented. The advantages of the composite skirts are introduced.
介绍了固体火箭发动机壳体裙的结构、用途及采用复合材料裙体的优点。
2
In this paper we employed the nonlinear finite element method to calculate the stress and bursting pressure of filament wound rocketmotorcase.
本文采用大变形有限元方法进行纤维缠绕固体火箭发动机壳体的应力及爆破分析。
3
The burst pressure of filament wound pressure vessels which is applied to solid rocketmotorcase and gas tank in industry is an important design parameter.