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1)  multi-tube rocket
多管火箭子母弹
1.
In this paper, on the platform of the anti-aircraft and anti-missile multi-tube rocket, the problems of electromagnetic radiation and EMI of fuze inductive settable system are discussed weightily.
本文以防空反导的多管火箭子母弹为平台,着重讨论引信感应装定系统的电磁辐射和电磁干扰问题,进行感应装定系统的电磁兼容性设计,以满足引信的战术技术指标要求。
2)  rocket cluster bomb
火箭子母弹
1.
The advantage of rocket cluster bomb shows that compared to the generalmulti-damage and anti-armor capabilities have increased several times, the moment thehigher firepower and greater intensity of the coverage, in a way, compensated for thedisadvantage that the rocket ammunition accuracy is not high.
火箭子母弹的优越性表现为较普通多用途炮弹在杀伤威力和反装甲能力均有数倍的提高,具有较高的瞬间火力密集度和较大的覆盖范围,在一定程度上弥补了火箭弹药精度不高的缺陷;在大量使用新型子母式火箭弹药的情况下,进一步提高子母弹综合毁伤效能具有十分重要的意义。
3)  shipborne shrapnel
舰载火箭子母弹
1.
During shipborne shrapnel firing on shore as oppressive weapon, the method of firing distribution affected the result of destroying and firing support directly.
舰载火箭子母弹对岸上目标实施火力压制射击时,火力分配方式直接影响毁伤效果和火力支援任务的完成。
4)  MLRS
多管火箭
1.
Research of Virtual Prototype Based on Launching Random Dynamic of MLRS;
基于发射随机动力学的多管火箭虚拟样机
2.
Simulation of Dispersion of MLRS by Using the Maximum Entropy Method;
应用最大熵法的多管火箭密集度仿真
3.
Simulation Analysis System for MLRS Initial Disturbance Based on Virtual Prototype;
基于虚拟样机的多管火箭起始扰动仿真系统
5)  multiple launch rocket system
多管火箭
1.
The analysis on dynamics of multiple launch rocket system(MLRS) are the premise and key for evaluating and improving the performance of MLRS.
多管火箭动力学分析是评估和提高多管火箭性能的前提和关键。
2.
A method of decreasing experimental ammunition consumption was studied with a systemic simulation method for a multiple launch rocket system.
采用系统仿真技术对某型多管火箭武器系统减少试验用弹量进行研究,首先给出确定1组非满管用弹量的方法,然后对满管和非满管情况分别建立以下模型进行仿真计算:建立燃气流模型,计算燃气射流冲击发射装置迎气正面的作用力和作用力矩;建立发射动力学模型,对发射过程建模和分析,得到炮口起始扰动的角位移和角速率;建立外弹道模型,即在发射动力学得到的火箭炮炮口参量下,进行火箭弹炮口扰动的转化,进而进行射击密集度的计算。
6)  mutiple launch rocket
多管火箭
1.
In order to understand distribution characteristics of firing range and intensity of mutiple launch rocket(MLR), sample mean value and variance distribution model of MLR falling points and their conditions of mutual independence were studied by means of multielement normal distribution and matrix analysis theory.
为了弄清楚多管火箭射程和密集度的分布特征,应用多元正态分布和矩阵分析理论,研究了多管火箭落点样本均值和方差的分布模型和它们相互独立的条件。
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