An integrated conceptual design software system for solid rocket motors SRMCAD is developed.
研制了一种固体火箭发动机集成方案设计系统软件SRMCAD。
This paper presents a method of optimum design for single-chamber double-thrust solid rocket motors.
本文讨论了单室双推力星形装药固体火箭发动机的结构优化方法。
In addition, this achievement provides the basis of integrative performance calculation for all kinds of solid rocket motors.
而且,这一成果为整个固体火箭发动机领域流场的一体化计算打下了基础。
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