摘要
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.
In this paper the method is put forward that the muzzle velocity deviation of charge lot is determined by thermal peribrmance 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.
关键词
武器系统
推进燃料
热物理学
热化学
初速度偏差
weapon system and application engineering
thermal physics and chenristry
propellant lot
muzzle velocity deviation
