1.
The Present Situation and Development of Servo System in Solid Missile
固体导弹伺服系统的现状和发展趋势
2.
A Study on Missile Plume Tracking and Localizing by Means of Forward Looking Infra-Red (FLIR)
红外探测阵列对固体导弹尾焰跟踪定位的研究
3.
Research on Key Technologies in Testing Assembly Line of Solid Missile Engine
固体导弹发动机装配检测生产线关键技术研究
4.
SPIRBM (Solid Propellant Intermediate Range Ballistic Missile)
固体推进剂中程弹道导弹
5.
Using parabolic trajectory of ballistic missile, surface to air missile with solid propellant can realize the aim of lesser weight and farther range.
地空导弹采用弹道导弹的抛物弹道技术，能够实现应用固体推进剂达到低质量远射程的目标。
6.
Fluid-structure interaction analysis of flow-induced elastic tube bundles vibration
流体诱导弹性管束振动的流固耦合分析
7.
Predominance of Ducted Solid Rocket Ramjet Applied to Airborne Missile
固体火箭冲压发动机在空空导弹上应用的优势
8.
Research on Robust and Adaptive Attitude Control System Design of Solid-propellant Ballistic Missile;
固体弹道导弹鲁棒及自适应姿态控制系统设计研究
9.
Viscoelastic Fractional Derivative Model and Its Applycation on Solid Rocket Motor;
粘弹性分数阶导数模型及其在固体发动机上的应用
10.
An numerical calculation method on cook-off of solid rocket motor of ship-based missiles
一种舰载导弹固体火箭发动机烤燃过程的数值计算方法
11.
Research of analysis method for storage life of SRM
舰上导弹固体火箭发动机贮存寿命的分析方法研究
12.
Abstract: Using parabolic trajectory of ballistic missile, surface to air missile with solid propellant can realize the aim of lesser weight and farther range.
文摘:地空导弹采用弹道导弹的抛物弹道技术，能够实现应用固体推进剂达到低质量远射程的目标。
13.
hard missile base
混凝土掩体导弹基地
14.
The Conflict of Attack and Defence System Between TBM and ATBM
地地弹道导弹武器系统攻防体系对抗
15.
Adaptive Parameter Estimation for Transverse Vibration of the Flexible Missile
弹性体导弹横向振动自适应参数估计
16.
Influence of Position Change of Projectile Pressure Center on Trajectory of Terminal Guidance Shell
弹体压心位置变化对末制导炮弹弹道的影响
17.
A fixed or movable airfoil used to stabilize an aircraft, a missile, or a projectile in flight.
安定翼，直尾翅用以稳定飞行中的飞机、导弹或发射体的固定式或活动式机翼
18.
New insight also was offered on Chinese solid rocket motor technology work, important for both missile and space launch applications.
研究还提供了对于导弹和航天发射都具有重要影响的固体火箭发动机技术工作。