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针对热动力鱼雷减速增程改装过程中出现的问题,对鱼雷的燃料各组分供应比例与航程之间的关系进行了分析计算,并提出了减速后获得较大航程的方法。
Aiming at the problems occurred in the conversion process of the PTO deceleration deceleration range, the relationship between the supply proportion and the flight distance of each component of the torpedo fuel is analyzed and calculated, and the method of obtaining the larger flight after the deceleration is proposed.