姿态控制推力器在飞行器上的应用  

The Application of Attitude Control Thruster in Flight Vehicle

作　　者：毛雪瑞[1] 杨树兴[1] 

机构地区：[1]北京理工大学机电工程学院,北京100081

出　　处：《弹箭与制导学报》2006年第2期13-15,共3页Journal of Projectiles,Rockets,Missiles and Guidance

摘　　要：姿态控制推力器(ACT)是飞行器控制系统的执行部件。在控制信号的作用下,ACT通过向飞行器外流场喷射高速燃气流为飞行器提供控制力。文中介绍了ACT的结构、优点以及ACT的工作原理,并简要分析了ACT内外流场的特征。The attitude control thruster （ACT） is the control component of the flight vehicle. With input of the control signal, the ACT could provide thrust to the flight vehicle by injecting jets into the outer flow field. In this paper, the advantages of the ACT are listed and its structure, properties and operating principle are briefly depicted. The characteristics of the outer flow field of the ACT are analyzed. Finally, some development trends of the ACT are discussed.

关 键 词：姿态控制推力器 射流元件 超音速射流 

分 类 号：TJ765.23[兵器科学与技术—武器系统与运用工程]