thruster的例句大全

The summary of various oscillation should have a clear physical mechanism of oscillation, give the research methods issue from domestic to foreign and indicate the existence of current problems of oscillations; The establishment of Hall thruster experiment system to measure high-frequency radiation.

综述应阐明各个频段振荡产生的物理机理，给出国内外对振荡问题研究的方法，指明目前振荡研究存在的问题；建立霍尔推力器内高频辐射实验测量系统。

Study on the Capability of Laser-Powered Heat Exchanger Thruster and the Launch System Project

激光供能换热器模式发动机性能及发射系统方案研究

How to applied chaos science to thruster motor of robot system involves two issues, that is, when chaos is useful need an anti-control of chaos, when it harmful need chaos control.

如何将混沌科学应用到机器人推进系统当中，这涉及到混沌有害时进行控制，混沌有益时进行反控制两方面的问题。

Meanwhile, the thruster arrangement, the control system configuration, and the thrusting force distribution of the AUV are introduced.

同时介绍了它的推进器布置、控制系统结构、推力分配等方法。

Based on the untethered AUV developed by our institute, this paper analyzes the navigation control and the position control methods of AUV. Meanwhile, the thruster arrangement, the control system configuration, and the thrusting force distribution of the AUV are introduced.

以成功研制的无缆自治水下机器人（AUV）为基础，对其航行控制和定位控制方法进行了较详细的分析.同时介绍了它的推进器布置、控制系统结构、推力分配等方法。

The results of static firing test shows that the thermal erosion properties, mechanical properties, tand thermal shock resistance of the C/ SiC composites can meet a demand for thermal-structure application in the area of Aerospace such as liquid rocket thruster.

试验发动机地面热试车结果表明，该C/SIC复合材料的力学性能、烧蚀性能和热震性能优良，可满足宇航工程中诸如液体火箭发动机推力室等对热结构材料的使用性能要求。

Design of orificed hollow cathode for 8-cm mercury ion thruster prototype

8cm汞离子推进器样机用小孔空心阴极设计

Hollow cathode for electron bombardment mercury ion thruster pulse ignition characteristics

汞离子推力器用的空心阴极脉冲点火性能

An Experimental Investigasion of the Hollow Cathode for Electron Bombardment Mg-Ion Thruster

用于电子轰击式汞离子推力器空心阴极的实验研究

Advanced agile missiles possess maneuverability, agility and accurate guidance performance by adopting thruster vector control or reaction control system thruster.

新型精确制导导弹为了获得更大的机动性、敏捷性和更高的命中精度，大多采用了推力矢量控制或反作用推力控制。

Ignition start-up course calculation and ignition charge mass selection of impulse micro-thruster Start up processes of D T burning in a tokamak reactor for different heating scenarios are studied.

微型脉冲推力器点火启动过程计算与点火药量选择研究了不同的加热功率沉积剖面对托卡马克反应堆点火启动过程的影响。

Experimental and numerical studies on 0.1 kW microwave plasma thruster were presented.

主要对0.1kW微波等离子体推力器进行了地面试验和数值模拟研究。

A Hall thruster, with its high-efficiency and high specific impulse, is one of the most important electric propulsion devices widely used for spacecraft propulsion such as attitude control, orbital transfer and deep space exploration missions in the future.

霍尔推力器作为一种等离子体装置，以其高效率高比冲等特点成为国际电推进领域的研究热点，广泛应用在姿态控制，轨道转移及将来的深空探测任务。

Application of Electric Drive Hydraulic Thruster Brake in Coal Belt Transport

电动液压推杆制动器在输煤皮带机上的应用

In order to reveal electromagnetic characteristics and interaction between electromagnetic field and high temperature ionized gas within arcjet thruster, improved modeling of electromagnetic field was developed and various numerical techniques were observed and studied.

为了揭示电弧喷射推力器内部电磁场特征及其与高温电离气体间的相互作用机理，建立了比较完善的电磁场模型，详细讨论了电磁场数值模拟方法及其计算效果。

Performance optimization is one of important facets for the investigation of laser thruster.

激光推力器性能优化是激光推力器研究的重要组成部分。

Investigation on head of novel chemical thruster for orbit maneuver

新颖机动变轨化学火箭发动机头部研究

Ground Ignition Test of an Orbit Maneuver H_2/ O_2 Thruster Based on Gas Dynamic Resonance Igniter

基于气动谐振点火器的氢氧变轨火箭发动机地面点火试验

Orbit maneuver hydrogen-oxygen thruster based on gas dynamic resonance igniter is a novel chemical propulsion technology especially prospective in space station application.

结合气动谐振点火器进行头部设计的氢氧变轨火箭发动机是一项新颖化学火箭推进技术，尤其适于空间站应用。

Hydrogen and oxygen orbital maneuver thruster, based on gas-dynamic resonance ignition, is a new liquid rocket propulsion technology, and is especially applicable to space station.

基于气动谐振点火技术的氢/氧变轨发动机是一项新型的液体火箭推进技术，尤其适用于空间站应用。