鸭式布局火箭滚转特性试验研究

Experimental Research of Rolling Characteristics on Canard-configuration Rocket

以某鸭式布局的简控火箭为研究对象,首先通过模型风洞试验获取了其气动特性参数,然后以此为基础重点对其滚转特性进行分析,给出了利用鸭舵实施火箭滚转控制的可行性方案,最后通过飞行试验进行了验证。

Rocket aerodynamic characteristic parameter is acquired through wind tunnel test, and the rocket rolling aerodynamic characteristic is analyzed, then obtain the feasible plan of rocket rolling control using canard-configuration mechanism. Afterwards, the experiment of flight test verification for this type of rocket is completed.