research rocket的例句大全

From SOUNDING-7 meteorological rocket to VEGA-3 high altitude research rocket& review the past thirty years since the first successful launch of SOUNDING-7 rocket

从探空七号气象火箭到织女三号高空研究火箭&我国实用探空火箭发射成功30年回顾

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Experimental research on the thrust chamber of tripropellant rocket engine

三组元火箭发动机推力室试验研究

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Research on kinematic control and flexible effects for a rocket launcher coupling system

弹－架耦合系统运动控制与柔性效应研究

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An Exploratory Research of Test Technique for Solid Rocket Motor Thrust Termination

固体火箭发动机推力终止试验技术探讨滚珠式推力终止装置可靠性研究

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Research on thermal protection for rocket electrical system's cable network

火箭电气系统电缆网热防护研究

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The research of thermal protection system for the ramjet combustor of the integral solid ducted rocket motor is an important component of the development of the solid ducted rocket motor.

补燃室热防护系统研究是飞航导弹固冲发动机研究的一项重要内容。

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Research on Working Process of Pasty Propellant Rocket Motor

膏体推进剂火箭发动机工作过程研究

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Technology research and improvement of ingot forming for rocket engine housing

火箭发动机毛坯冲压工艺的改进研究

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Research on Attitude Control Strategy of Glide Range Extend Rocket

滑翔增程火箭弹的飞行姿态控制方法研究

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Research on the data processing method of solid propellant rocket engine plume temperature

一种测量固体火箭发动机羽焰温度的数据处理方法研究

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Evaluation research of infrared radiation characteristics of solid rocket motor exhaust plume

固体火箭发动机尾焰红外辐射特性预估研究用水龙头把水射向火焰

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Yao Ming in National Sports Team and Rocket Attack Technique and Tactics Comparison Research

姚明在国家队与火箭队进攻技战术的比较研究

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The Aerodynamic Design Research of Gas Vane of Solid Rocket

固体火箭燃气舵气动设计研究

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Research on Optimal Algorithm of Glide Range Extend Rocket

滑翔增程火箭弹弹道优化算法研究

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Research of damage mitigating control of thrust chamber based on fuzzy logic reasoning for liquid propellant rocket engine

基于模糊推理的液体火箭发动机推力室减损控制研究

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Research on Assessment of Battlefield Damage by a Certain Rocket Launcher Based on PDA

基于PDA的某型火箭炮战场损伤评估研究

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The paper research fire angle of the projectile, firing time of the rocket motor, assisted time of the rocket motor, flying attitude of the glide phase and the terminal phase guidance law to add the projectile firing range.

在建立的模型的基础上，深入研究了炮弹的射角、火箭发动机的点火时间、火箭发动机的助推时间、滑翔段的飞行姿态以及末段制导律等对炮弹的射程及性能的影响。

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Research on Test Data Processing Scheme of Strapdown Inertial Measurement Unit Based on Rocket Sled

捷联惯组火箭橇试验数据处理方案研究惯性测量装置火箭橇试验模拟导弹飞行过载方法

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Research on Flight State Calculation for Rocket Launched Marine Buoyant Apparatus

火箭发射水面浮具飞行状态计算研究

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Review of combustion instability testing research on liquid propellant rocket engine

液体火箭发动机燃烧不稳定性试验研究简述

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