1.
Electrical Property Parameter Computation and Simulation of Missile Radome Material
导弹天线罩材料电性能参数计算与仿真
2.
The fairing of a multi-warhead missile requires an all-weather, omni-bearing operating environment;
多弹头导弹整流罩要求全天候、全方向的工作环境。
3.
Beam pointing error of a radome
天线罩波束指向误差
4.
Reflected power coefficient of a radome
天线罩功率反射系数
5.
Broadband Omnidirectional Antennas and Electromagnetic Analysis of Radomes;
全向宽带天线及天线罩电磁特性研究
6.
Can this apparent dish-body coupling unstabilise the guidance loop?
这种明显的天线-弹体耦合，能否导致制导回路不稳定？
7.
The radome causes an angular displacement of the tracking aerial polar diagram.
天线罩使跟踪天线的极图产生了角位移。
8.
Analysis of an Optimized Conjugate Gradient Algorithm for Antenna-Radome System
天线-天线罩系统分析的优化共轭梯度算法
9.
Analysis of Characteristics of Complex Structured Radome and Its Optimization with Genetic Algorithm;
复杂结构天线罩电性能分析与GA优化
10.
Analysis of Key Factors Effect on the Performance of Radome
影响雷达天线罩性能的主要因素分析
11.
Radiation Characteristics of a Two-Dimensional Radome-Enclosed Phased Array Antenna
二维带罩相控阵天线的辐射特性研究
12.
infrared seeker
红外线寻的制导导弹(或其弹头)
13.
What deserves special mention is that a distinct difference exists between the design technology of the fairing on a carrier rocket and that of a multiple-warhead missile.
更需要指出的是，运载火箭整流罩的设计技术与导弹多弹头整流罩设计技术存在显著的不同。
14.
Can this apparent dish-body coupling unstabilize the guidance loop?
这种明显的天线-弹体耦合能使制导回路不稳定吗？
15.
An In-flight Calibration Method of Ballistic Missile SINS
弹道导弹SINS空中在线标定方法
16.
Missile Geo-Location Using INS and Dual-Antenna Missile-Borne SAR
INS/双天线弹载SAR组合弹体定位技术
17.
A transmission line between an antenna and a transmitter.
传导线天线和传导器之间的传导线
18.
The radome was hinged to permit easier access to the radar.
雷达天线罩以铰链方式安装以便于检修雷达。