spin-stabilized rocket

The influence of double-push accelerated velocity, spin-rate regularity and unfolding fins on air rocket dispersion and the mechanism of decreasing of air rocket dispersion are also studied respectively.

分别研究了双推力加速度，转速规律和尾翼延时张开，对地面火箭弹和航空火箭弹散布的影响，以及减小航空火箭弹散布的机理。

It was found that the combustion synthesis is characterized by a nonsteady combustion mode, which leads to oscillatory and spin motion. Study on the Optimum Spin Motion of Uncontrolled Rocket

其燃烧模式为振荡燃烧及螺旋燃烧。无控火箭最优自转运动初探

This paper takes a large slenderness ratio spin rocket with a low spin velocity for example, and the launch dynamic behavior of the system is investigated when there is a clearance between the missile and the launcher.

以大长径比低速旋转火箭为例，探讨弹-架间隙非线性特性对不同发射装置系统的动力响应的影响。

Study on the Optimum Spin Motion of Uncontrolled Rocket

无控火箭最优自转运动初探

Also, spin rate coupling with structural damping ratio and other structural parameters have a significant influence in aeroelastic dynamic instability for spinning rocket.

旋转速率与结构阻尼及其他结构参数对气动弹性动态稳定性影响也比较显著。