1) Image of rocket
火箭弹图像
2) rocket bomb
火箭弹
1.
The traditional rocket bomb of blasting for dredging the jam of mine_shaft is introduced.
现介绍溜矿井疏堵爆破输送炸药包的专用工具———传统火箭弹、改进的安全火箭弹以及新开发准确度高的浮球炸药包。
2.
It is rather difficult to select environment available to design for rocket bomb fuze,especially low-speed rotating rocket bomb time fuze.
对于火箭弹引信,在设计时选取可利用的环境相当困难,尤其是低旋的火箭弹时间引信。
3) rocket
[英]['rɔkɪt] [美]['rɑkɪt]
火箭弹
1.
Multi-disciplinary design optimization on conceptual design of rockets;
火箭弹概念设计的多学科优化设计方法
2.
Research on constructing surrogate model of rocket aerodynamic discipline;
火箭弹气动学科代理模型构建方法研究
3.
Study on the LEMP Radiation Effect to Rocket Electric Ignition System;
某型火箭弹电点火系统雷电辐照效应研究
4) rocket projectile
火箭弹
1.
Research on detection of the rotating speed of a long range rocket projectile based on shortwave signals;
基于短波信号的远程火箭弹转速探测方法的研究
2.
The paper presents a method for measuring the rotating speed of a long range rocket projectile by using short wave signals.
提出一种利用短波信号进行远程火箭弹转速测量的方法,利用弹丸在旋转、飞行过程中,由于接收点所处位置的不同,接收的短波信号幅值会呈规律性变化,通过提取变化周期即可测得弹丸转速。
3.
The main factors influencing the safety of rocket projectile detection were summarized through analysis of the characteristics of rocket projectile detection and reliability.
在分析火箭弹检测的特点和安全性特征的基础上,归纳了影响火箭弹检测安全性的主要因素。
5) rocket depth charge
火箭深弹
1.
The rocket depth charge is the usual weapon to intercept the torpedo on the warship.
火箭深弹是水面舰艇拦截鱼雷的常用武器,为提高火箭深弹拦截鱼雷的概率,提出了子母深弹的概念,将地面火炮中常用的子母弹技术应用于深弹反鱼雷攻击中,通过分析子母弹的散布特性,来比较子母深弹和火箭深弹毁伤鱼雷的效能,并通过Monte-Carlo法仿真了这一过程,分析了影响子母深弹的毁伤概率的因素。
2.
Now the fire range and fire precision of rocket depth charge has been improved,and it will make the source of the rocket depth charges wasted and affect the hit probability raised if we still use the old fire strategy.
火箭深弹射程与射击精度提高后 ,如再沿用以固定发射间隔 ,对同一瞄准点齐射的方法对潜射击会造成资源的浪费 ,影响毁伤概率的提高。
6) rockets
[英]['rɔkit] [美]['rɑkɪt]
火箭弹
1.
This paper presents the basic theory of the simple-control and guide system of long-distance rockets and the inertial components-liquor dynamic gyro.
为了解决这一问题而又不使成本大幅增加,对火箭弹进行简易制导是一种行之有效的办法。
2.
The basic principle and realizing process to construct the Wrap-Around-Fins rockets’ parametric 3D model are described in detail.
对卷弧翼火箭弹参数化建模的基本原理和实现步骤进行了详细说明。
3.
The rocket numbers prescribed in current China national army criterion for the use in high and low temperature environment test don\'t adjust to the design test for costly rockets.
针对现有国军标规定的高、低温环境试验用弹量难以适用昂贵火箭弹定型试验的需要,提出了应用专家经验和Bayes方法的高低温环境下减少试验用弹量的试验方法。
补充资料：高光谱分辨率遥感图像及图像光谱信息提取
高光谱分辨率遥感图像及图像光谱信息提取
高光谱分辨率遥感图像及图像光谱信息提取 郑兰芬供稿
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