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本方论述了固体火箭飞行器初步设计的数值优化方法。该方法以整体观点出发同时考虑了内弹道学和外弹道学的问题。采用该方法将由于工作量的显著减少而大大缩短设计过程,并且极易进行灵活的设计。
This paper discusses the numerical optimization of the initial design of solid rocket vehicle. The method considers both the internal ballistics and the external ballistics from a holistic point of view. With this method, the design process will be greatly shortened due to the significant reduction in workload and the design will be extremely flexible.