1) long-range rocket
远程火箭<火>
2) long-range rocket
远程火箭
1.
After the attitude being stabilized, restraining the range dispersion of long-range rocket becomes the more important problem.
实现了姿态稳定后,抑制远程火箭的纵向散布上升为提高其射击效能的主要问题。
2.
Aiming at the problem that long-range rocket\'s testing range is different from the calculating range,a new viewpoint was advanced that there are differences between pitching and yaw of equatorial damp moment when the attacking angle is big.
针对远程火箭试验射程与计算射程不相符的问题,提出了大攻角下应考虑赤道阻尼力矩章动阻尼与进动阻尼特性的不同,推导了这种不同与攻角的关系,用奇点理论与振幅平面方程推导了在这种非对称赤道阻尼力矩作用下产生极限圆锥运动的条件,通过数值计算进行了验证。
3) long-range rocket
远程火箭弹
1.
Attitude stabilized technology is very us ef ul to reduce the dispersion of long-range rocket, but the range dispersion of a ttitude stabilized rocket is not very satisfactory still.
在主动段进行姿态稳定是提高远程火箭弹射击密集度的有效技术措施 ,实施了姿态稳定后 ,火箭弹的纵向散布仍然偏大 。
2.
With numerical simulation, reasons of technical dispersion for long-range rockets resulting from various factors of disturbance are analyzed.
通过数值仿真分析了弹道风、质量偏心、推力偏心、初始扰动等各种扰动因素引起远程火箭弹落点技术散布的机理,指出火箭弹落点散布主要来源于主动段,且主动段终点速度矢量的方向散布是造成落点散布的关键。
4) long range rocket projectile
远程火箭弹
1.
The paper analyses the characteristic of long range rocket projectile and the classification of the target,describes the basic elements of task allocation,sets up the mathematics matching model of long range rocket projectile and its attacking target and analyses the model with genetic algorithm.
文中分析了远程火箭弹特性及其打击目标的分类;论述了任务分配的基本要素;建立了远程火箭弹与其火力打击目标匹配的数学模型,并引入遗传算法对其进行分析,为解决远程多管火箭炮系统在火力打击中的任务匹配问题提供了一种有效方法。
2.
Performances and fault characteristic of long range rocket projectile weapon systems in various circumstance is analyzed.
针对远程火箭弹武器系统在不同环境条件下试验的特点 ,分析了远程火箭弹武器系统在不同环境条件下的性能特点及故障特性 ,探讨了其失效模式 ,建立了故障树 ,确定了其检测内容 。
5) long-range rocket launcher
远程火箭炮
1.
Meteorology condition is of great influence for shooting precision of certain type of long-range rocket launcher, this paper use the error-analyses method to deal with this problem.
针对远程火箭炮武器系统射击精度问题,运用误差分析法探讨气象条件对远程火箭炮武器系统射击精度的影响。
6) long range MLRS
远程多管火箭
1.
According to the up-to-date theories from the launching dynamics and the multi-body system dynamics and utilizing the established simulation system which can precisely depict the motion law of the long range MLRS,The relationship of the shot accuracy between short,middle and maximum range can be quantitatively defined,so an it can be used to realize the reduced computation of different range.
文中根据发射动力学和多体系统动力学最新理论,利用建立的可以精细刻画远程多管火箭运动规律的仿真系统,确定了远程多管火箭中、小射程射击精度与最大射程射击精度的定量关系,从而可以实现不同射程射击精度的折算。
补充资料：固液混合火箭推进剂(见火箭推进剂)
固液混合火箭推进剂(见火箭推进剂)
solid-liguid hybrid rocket propellant
guye hunhe huoiian tui)in)i固液混合火箭推进剂(s olid一Iiguid hy-brid rocket proPellant)见火箭推讲齐，}_
说明：补充资料仅用于学习参考，请勿用于其它任何用途。
参考词条