rocket engine
美 
英
- un.火箭发动机
- 网络火箭引擎；火箭动力机；火箭发动机试验
英汉解释
英英解释
例句
Unlike a rocket engine, the jet engine, as you know, is an "air breather" .
正如你们所知道的，这种喷气发动机与火箭发动机不同：它是“空气喷气发动机”。
This alone is enough to give the disk lift and with the addition of the rocket engine its vertical acceleration would be extremely rapid.
仅此是不够的，让磁盘升降机及与增补的火箭发动机，其垂直加速度会非常迅速。
The rocket engine , with its steady roar like that of a waterfall or a thunderstorm , is an impressive symbol of the new space age .
火箭发动机以其类似于瀑布或大雷雨的持续轰鸣给人以深刻印象，成为太空新时代的象征。
The missile uses active radar homing and is powered by a solid rocket engine (with a solid rocket booster).
导弹使用主动雷达引导和动力由一台固体火箭发动机（使用一台固体火箭助推器）提供。
"So many bits of the rocket engine fall off that it would be dangerous to aircraft if [flights] were allowed. "
“会有那么多的火箭发动机碎片脱落，如果允许（航班）起飞，那么对飞机来说将是危险的。”
The forward - directed force developed in a jet or rocket engine as a reaction to the high - velocity rearward ejection of exhaust gases.
推力，侧面压力喷气发动机或火箭发动机产生的作为高速向后排出的气体的反作用力而向前推动的力量。
The rocket engine carries with it the oxygen of its own .
火箭发动机自带氧气。
Theory Of Operation: A rocket engine thrusts against a water filled syringe. This produces pressure readings on a connected pressure gauge.
理论的运作：一火箭发动机推力对一个充满水的注射器，这产生的压力读数，就一连接压力计。
The feed system of a rocket engine may be the cause of undesirable oscillations .
火箭供应系统可能是有害的振源。
Rotor dynamic is one of the most complicated problems in development of LOX turbopump of liquid rocket engine.
转子动力学问题是液体火箭发动机研制中最复杂的问题之一。
Another unconventional design element, the hybrid rocket engine that powers the suborbital vehicle, provides unique operational options.
另一个异于传统的设计要素，是提供次轨道载具动力的混合式火箭引擎，它能提供独特的操作选择。
for liquid propellant rocket engine , it is an important condition for effective combustion that propellant be evaporated and mixed quickly.
在液体火箭发动机中，推进剂组元迅速而高效的气化和混和是产生高质量燃烧所必须的重要条件。
The turbopump is an important part of the liquid rocket engine, whose task is fuel transporting.
涡轮泵是液体火箭发动机的重要组成部分，主要担负燃料的输送任务。
The mathematical models of the static characteristics of the full-flow staged combustion cycle rocket engine were presented.
建立了全流量补燃循环发动机的静态特性的数学模型。
It is an important and basic issue to choose monitoring parameters of Liquid propellant Rocket Engine(LRE) monitoring system in ground test.
确定监测参数是液体火箭发动机地面试验监控系统的一个重要而基础的问题。
And, oil painter Robert McCall imagines the sight of the rocket engine firing to propel the lunar lander back to earth.
此外，油画家罗伯特麦考想象的火箭发动机点火推动月球着陆器返“u200b”u200b回地球景象。
Russian teacher of that time, Konstantin Tsiolkovsky, decided that a rocket engine could provide power for a space vehicle.
康斯坦丁齐奥尔科夫斯基，俄罗斯老师，当时的决定，可以为航天器提供电力的火箭发动机。
The detonation wave ignition technique is suitable to synchronization ignition of multi-chamber liquid rocket engine.
爆震波多管点火技术适合用于多燃烧室液体火箭发动机的同步点火。
For example, the rocket engine seal life just a few minutes, but require a short period of time does not leak.
例如，火箭发动机的密封寿命只需几分钟，但要求短时间内绝对不漏。
Seen from above, the spacecraft Tycho Brahe is settled onto the HEAT-1X rocket engine.
从高空往下看，航天飞机第谷·布拉赫号正被安置到热火-1X火箭发动机上。
A rocket engine typically goes faster but has to carry its own supply of oxygen.
火箭发动机通常使飞行更快，但需要自携氧气。
For one thing, they simplify the design of a rocket engine.
首先，它们可以简化火箭发动机的设计。
The paper introduces a new method of measuring combustion time with CAT technique for solid rocket engine.
介绍一种应用CAT技术确定固体火箭发动机燃烧时间的新方法。
Nonlinear regression algorithm based on quantum genetic algorithm was put forward to and applied in liquid rocket engine fault detection.
提出一种基于量子遗传算法的非线性回归算法，并应用于液体火箭发动机故障检测中。
It introduced the physical simulation model based on artificial neural networks on solid rocket engine milling process.
介绍了基于人工神经网络的固体火箭发动机药柱铣削加工过程物理仿真模型。
How can a rocket engine that generates 5, 000 degree steam and 13, 800 pounds of thrust form icicles at the rim of its nozzle?
一个能制造出5000度高温蒸汽和13800磅推力的火箭推进器，是怎样使喷口边缘结冰的呢？
And rocket engine function test occupy the important status in the all kinds of tests of rocket.
而火箭发动机性能测试在火箭武器各类试验中占有重要地位。
A rocket engine can work in space where there is no air.
火箭发动机能在没有空气的太空中工作。
Vortex Injection provides a form of swirl or cyclone combustion for a rocket engIne similar to systems often employed In Industrial furnaces
涡流喷射在火箭发动机中产生一种涡流或旋涡形式的燃烧，与工业炉中常采用的系统相似。
Implementation of A High Frequency Measuring System for the Testing of Combustion Instability Study of Tripropellant Rocket Engine
三组元发动机不稳定燃烧研究试验高频采集系统的实现
Modeling and Dynamic Analysis of the Mass Flow Control System Used for Rocket Engine
用于火箭发动机的低温流量控制系统建模及动态特性分析
Plume temperature measurement of a solid propellant rocket engine using multispectral thermometry
基于多光谱法的固体火箭发动机羽焰温度测量
Application of immunity strategy for the study of the static characteristics of a rocket engine
免疫算法在火箭发动机静态特性研究中的应用
Principle and design of simulation test for acoustic characteristics of liquid rocket engine chamber with a single injector
液体火箭发动机单喷注器燃烧室声学特性模拟实验原理及实现
Numerical simulation of the temperature distribution in the turbo-pump system of a rocket engine during gliding
滑行过程中火箭发动机泵系统各构件温度数值模拟
The Design and Implementation of a Variable Thrust Liquid Propellant Rocket Engine Control System
一种大范围变推力液体火箭发动机控制器的设计及实现
Numerical Simulation and Experimental Study of Viscous Flow Field in Rocket Engine propulsion
火箭发动机推力室粘性流场数值模拟及实验
Fundamental study of fault monitoring and diagnostic technology of liquid rocket engine
液体发动机故障检测与诊断中的基础研究问题
A Comprehensive Numerical Model for Initial Propellant Temperature Effecting Liquid Rocket Engine Combustion Stability
推进剂初始温度影响液体火箭发动机燃烧稳定性的数值模型
Kinematics Analyzed of a Virtual Axis Machine Tool Applied in Solid Rocket Engine Grain Machining
固体火箭发动机药柱整形虚拟轴机床的运动学分析
