单元推进剂液滴在高温高压下的微爆现象观测  

MONOPROPELLANT DROPLET MICROEXPLOSIONS UNDER HIGH PRESSURE AND TEMPERATURE

作　　者：余永刚[1] 金志明[1] 

机构地区：[1]南京理工大学动力工程学院,江苏南京210094

出　　处：《高压物理学报》2000年第4期302-308,共7页Chinese Journal of High Pressure Physics

基　　金：国家自然科学基金!(596760 4 4 )

摘　　要：利用挂滴装置和高速摄影系统研究了单元推进剂LP184 6液滴在 0 2～ 4 0MPa、673～973K工况下的微爆特性。观察到液滴在不同环境压力和温度下的 3种微爆模式 ,即液滴在着火前的轻度破碎、液滴在燃烧时的部分破碎和全部爆碎 ,并给出了微爆过程的特征照片 ,定量测试了液滴微爆延迟期、微爆温度和微爆直径与环境压力、温度的关系。初步分析了液滴微爆机理 ,认为第一种微爆机理主要是水组分的过热 ,第二、三种微爆机理是液相化学反应。研究结果对控制LP184 6燃烧稳定性和指导液体发射药火炮内弹道设计均有参考价值。The properties of microexplo sions of monopropellant LP1846 droplets in ambient conditions of 0.2～4.0M Pa,673～973K were investigated using a suspended droplet apparatus and a hig h speed camera.Three modes of microexplosions,i.e.,slight fragmentation of dropl ets before ignition,part and full fragmentations of droplets during burning peri o d,were observed under different pressure and temperature,and characteristic phot ographs of droplet microexplosions were given.Microexplosion delay time,temperat ure and diameter of droplets were also measured quantitatively.Droplet microexpl osion mechanisms were analyzed primarily.It is suggested that the mecha nisms of the three modes are the overheating of water component for the first m ode, and liquid phase reactions,respectively.The results are of reference value to control combustion stability of LP1846 and design interior ballistics of regenerative liquid propellant guns.

关 键 词：液滴微爆 液滴燃烧 液体推进剂 液体发射药火炮 超高速发射 单元推进剂 微爆延迟期 微爆温度 微爆直径 

分 类 号：TQ562[化学工程—炸药化工] V511[航空宇航科学与技术—航空宇航推进理论与工程]