spin rocket

Transient responses of a flexible spin rocket launch system with a supersonic jet

高速喷流下的柔性旋转火箭发射系统瞬态响应

The test analysis of affection of spin rocket projectile ′ s unbalance to the dispersion

动静不平衡度对旋转火箭弹散布影响的实验分析

As the increase of motor size and the time of motor operation, the spin stabilized solid rocket propelled space vehicles performed the unpredictable nutation instability.

自旋稳定固体火箭发动机飞行器随着发动机尺寸的增大，工作时间的增长，在发动机工作末期出现了不可预见的不稳定性运动。

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。

An investigation on the burning rate performance of low burning rate solid propellant applied to spin rocket motor

高速旋转固体发动机低燃速推进剂燃速性能的研究

Spatial Dynamic Response of Flexible Spin Rocket at Launch

柔性旋转火箭发射时的空间动态响应

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。

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。

Study on the Optimum Spin Motion of Uncontrolled Rocket

无控火箭最优自转运动初探

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