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Determination of Muzzle Velocity Deviation of Propellant Lot by Thermal Physical and Chemical Performances of Propellant
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作者 Liu Yixin Wang Guiyu 《工程科学(英文版)》 2005年第4期16-19,共4页
In this paper the method is put forward that the muzzle velocity deviation of charge lot is determined by thermal performance or component and content of propellant. Live firing or other experiments can be left out by... In this paper the method is put forward that the muzzle velocity deviation of charge lot is determined by thermal performance or component and content of propellant. Live firing or other experiments can be left out by using this method and its accuracy is rather high. 展开更多
关键词 武器系统 推进燃料 热物理学 热化学 初速度偏差
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