thruster的例句大全

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。

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Without the thruster, the washing-machine-size Philae would have to rely on ice screws on its landing legs and the harpoons to anchor it to the comet.

如果没有那个推进器，洗衣机大小的菲莱就只能依靠着陆装置上的冰锥和鱼叉来抓牢彗星表面。

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When design the control method of long-time cycle movement, whiff thruster is used to assistant the control system.

其中长周期运动控制律设计时，结合了喷气推力控制来辅助偏置动量控制；

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Status and development trend of concept studies on laser propulsion thruster

激光推进器概念设计研究现状及发展趋势

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Design of a Liquid Propellant Feeding System for Laser Propulsion Thruster

激光推力器液体工质注入系统设计

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The functions of the hollow cathode for electron bombardment mercury ion thruster and its requirements are described.

本文叙述了空心阴极在电子轰击式汞离子推力器中的功能、推力器对空心阴极的要求。

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Influence of linear nozzle structure on impulse coupling coefficient of laser thruster

线性喷管构形对激光推力器冲量耦合系数的影响

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The Application of CAN Bus in the Undulated Biomimetic Thruster

CAN总线在波动仿生推进器中的应用

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The influence of catalyst porosity, length, specific area and Sherwood number to the transient and stable performance of the thruster were studied and analyzed.

分析和研究了催化剂的孔隙率、长度、比表面积、传质Sh对推进系统的瞬态及稳态性能的影响。

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Research on n_2o_4/ mmh thruster if f1 ( 0).

四氧化二氮/一甲基肼推力室研制＞0，（1一E）。

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Combustion Characteristics of Thruster with High Burning Rate Pyrotechnics

高燃速烟火型做功器件燃烧特性研究

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Microwave plasma thruster ( MPT) was applied to the sub system of DFH 3 satellite to complete its orbit transfer ( OT) and north south station keeping ( NSSK).

将微波等离子推力器（MPT）应用于东方红三号（DFH3）卫星的推进子系统，完成其轨道转移和南北位置保持任务。

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Mission and System Optimization Analysis of Geosynchronous Satellite Based on Arcjet Thruster

基于电弧推力器的地球同步轨道卫星系统任务设计与优化分析

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An on-off control law of a divert thruster for an exo-atmospheric interceptor during its terminal course was put forward.

针对处于末段飞行的大气层外拦截器设计了轨控发动机开关控制律。

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Experimental Results of the Impact of an Ion Thruster Plasma on Microwave Propagation

离子推进等离子体与微波传播碰撞的实验结果

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Based on a comprehensive investigation of international electric propulsion development in period from 2001 to 2005, the most of technical progresses and applications both in ion thruster and Hall thruster are reported respectively, and main directional development tendencies are analyzed briefly as well.

在系统调研2001年至2005年技术发展的基础上，综述了国外离子和霍尔电推进的最新进展和飞行应用情况，分析了当前离子和霍尔电推进技术的主要发展趋势。

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Because of the safety and cost advantage, paraffin based fuel hybrid rocket can become available as cheap reusable rocket thruster in 5~ 10 years.

固液混合火箭具有安全、价廉等优点，石蜡基燃料的固液混合火箭有可能在5～10年内研究成功并应用于实际，成为一种廉价的可重复使用火箭助推器。

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The key component of the homogeneously catalyzed micro monopropellant thruster is its micro thrust chamber, which consists of the catalytic reaction tank and the micro nozzle. The impulse output resolution of the experimental prototype is better than 80 μ Ns.

同相催化的单组元液体推进器，其关键部件是微小型推力室，包括催化反应腔和喷管等结构，试验样机的冲量输出分辨率优于80μNs。

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Based on this method, the plasma particle simulation of ion thruster optics is carried out by PIC method, so that the feasibility of applying the linked list method to the particle simulation is validated.

使用基于链式存储结构的PIC方法对离子发动机光学系统进行了粒子模拟，验证了链式粒子信息存储方法在粒子模拟中的可用性。

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test of starting and maneuver: control bow thruster on bridge console and starboard & port wing console respectively.

起动和操纵试验：在桥楼控制台和右舷及左舷翼控制台分别控制艏侧推。

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