平飞固体火箭助推器设计

The booster design on flat flight solid rocket

介绍平飞固体火箭助推器的设计,重点是固体助推器主要参数的确定和助推器壳体的传热分析,给出具体算例,并与试验进行比较,结果表明设计是正确的。

The booster of a flat flight solid rocket is introduced. The focal points of introduction are to establish the main parameters of the solid rocket booster and the heat transfer analysis of the booster case. The practical example is given and its design parameters are compared with its tested results. It is indicated that the design and analysis methods are correct.