As the tailcone is removed we can see the thruster cones.
当尾锥被移除时，我们可以看到推进器锥。
The thruster design requires that the total volume of the propulsion system be less than 10 percent of the CubeSat.
这个推进器设计规定了推进器系统的总体积不超过立方体卫星的10%。
NASA developed a similar engine for its Deep Space 1 Mission, launched in 1998, but the new thruster has advantages.
NASA在1998年所发射的“深空一号”也曾使用类似的引擎，但相较而言，这个新型的推进器有自己的优势。
But safety rules prohibit the ships from remaining in space for more than 200 days, since their batteries can lose power and corrosive thruster fuel can degrade rubberized seals.
安全守则规定这些飞船不能暴露在宇宙空间中超过200天，因为电池会流失能量和推进器燃油会腐蚀橡胶密封。
The undulated biomimetic thruster is a new-style underwater thruster which is based on fish bionics.
波动仿生推进器是一种依据鱼类仿生学原理设计的新型水下推进器。
More visible thruster particles.
更明显的推进器粒子。
本船没有侧推器。
我们船有艏侧推器。
Do you have bow thruster or stern thruster?
你们船有艏侧推器还是艉侧推器？
The nozzle is one of the most important parts a laser thruster .
喷管是激光推力器的重要组成部分。
The several key technologies of laser micro-thruster are discussed as well.
讨论了激光微推力器需要解决的几个关键技术问题。
The attitude control thruster (ACT) is the control component of the flight vehicle.
姿态控制推力器(act)是飞行器控制系统的执行部件。
The establishment of Hall thruster experiment system to measure high-frequency radiation.
建立霍尔推力器内高频辐射实验测量系统。
This interval t1 is sometimes called the circuit-commutated-recovery time of the thruster.
这间隔时间t1有时叫半导体闸流管的电路换向恢复时间。
Propellant feeding system is indispensable to laser propulsion thruster with liquid propellant.
工质注入系统是液体推进剂激光推力器必不可少的一个组成部分。
The principle and research status of pulsed plasma thruster (PPT) were put forward in this paper.
论述了脉冲等离子体推力器（PPT）的工作原理和研究状况。
It shows filter could control the interference conduction from Hall thruster to its power supply.
发现滤波器能够有效地抑制干扰在霍尔推力器与电源间传播。
The results are very useful to design nozzle structure of laser thruster that works in air-breathing mode.
研究结果对于吸气式激光推力器的喷管构形设计具有指导意义。
The bow thruster to be equipped with a brake to avoid the turning of the propeller and motor during sailing.
艏侧推上应安装有刹车以防止航行时螺旋桨和马达发生转动。
Hydrazine decomposition thruster with canted nozzle is being more and more utilized in space propulsion system.
折角喷管肼分解发动机在空间推进系统正得到越来越多的应用。
The results can provide useful information for the design and experiment of electron cyclotron resonance thruster.
数值模拟结果可以为推力器的设计和实验研究提供有用信息。
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。
The experimental study of thruster plasma discharge parameters on the bridge of the impact of high-frequency radiation.
实验研究推力器放电参数对等离子体桥区高频辐射的影响。
This paper discusses the problem of detumbling a rigid spacecraft with an incomplete configuration of one sided thruster.
本文讨论了以非完整配置的单向推力器系统为执行机构时，刚性航天器的去翻滚控制问题。
The mechanism of electron near wall conduction (NWC) is one of the most important physics problems for thruster performance.
电子近壁传导是影响霍尔推力器工作性能的关键物理过程之一；
The structural design and fabrication process of the thruster, as well as the approach of propellant injection are presented.
给出了推进器的结构设计、工艺流程，以及推进剂加注方法。
The major function of DP system is to automatically control of a vessel's position and heading via precise thruster commands.
通过精确的推进命令自动控制船舶的位置和航向是动力定位系统的主要功能。
A control scheme is proposed, in which liquid engine of constant thrust and impulse thruster are chosen to achieve hover task.
提出一种近月面定点悬停的控制方案，选用常推力液体发动机和脉冲式发动机实现悬停任务。
For the finite propulsion reentry guidance, the conventional closed-thruster equation based on open-loop control loses its way.
解决有限推力模型的再入飞行器初制导问题，利用传统开环控制的关机方程达不到要求的精度。
For the finite propulsion reentry guidance, the conventional closed-thruster equation based on open-loop control loses its way.
解决有限推力模型的再入飞行器初制导问题，利用传统开环控制的关机方程达不到要求的精度。
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