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.
出处
《弹箭与制导学报》
CSCD
北大核心
2006年第2期13-15,共3页
Journal of Projectiles,Rockets,Missiles and Guidance
关键词
姿态控制推力器
射流元件
超音速射流
attitude control thruster
fluidic amplifier
supersonic jet
