1、

after arriving at the moon, subsequent thruster firings will circularize the probe's orbit at an altitude of approximately 124 miles.

到达月球后,后续的推进器将点火进入约124英里的轨道。

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2、

application of the electric-powered thruster in the complex car arrester

电动推杆在复式阻车器上的应用

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3、

mission numerical optimization for geosynchronous satellite using microwave plasma thruster

基于微波等离子推力器的地球同步轨道卫星任务优化计算

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4、

this paper presents the research and development work on series resonant ccps applied to pulsed plasma thruster (ppt).

本论文介绍了应用于脉冲等离子体推进器的串联谐振电容器充电电源的研制。

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5、

the operating principle and characteristics of the main components and subsystems of ion thruster, including the ion optic system, hollow cathode, ionization chamber, neutralizer etc. are analyzed and discussed. the development trend of ion thruster and its key technology is indicated.

介绍了离子发动机的基本原理与结构,分析了离子发动机系统主要部件包括离子光学系统、空心阴极、电离室、中和器等的工作原理与特性,指出了离子发动机的发展趋势。

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6、

In this study, the SST k-ω turbulence model was used to simulate the coupled whole field for the transpiration cooling of a thruster in a liquid O2/ H2 propellant rocket engine.

本文选用SST K-ω湍流模型对采用烧结多孔介质进行发汗冷却的液体O2/H2火箭发动机推力室进行了全场耦合数值模拟研究。

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7、

The Research about Inner Magnetic Pole Etched of Cylindrical Hall Thruster

圆柱形霍尔推力器的内磁极刻蚀研究

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8、

the effect of integrating azipod and bow thruster on ship maneuverability

全方位推进器与首侧推器综合作用对船舶操纵性能的影响

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9、

regenerative cooling of the pressure-fed thruster with low-pressure chamber

挤压式低室压推力室再生冷却问题

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10、

a cosine phase shifter is applied in phase shifting circuit to meet the possible maximum trigger current and voltage of thruster.

移相线路中配有与弦移相器以满足可控硅整流器最大可能触发电流和电压。

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11、

a review of the micro thrust measurement for pulsed plasma thruster

脉冲等离子体推力器微推力测试技术的述评

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12、

the pulsed plasma thruster for propeller in small and micro satellite

用于微小卫星推进装置的脉冲等离子体推力器

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13、

review of pulsed plasma thruster

脉冲等离子体推力器研究综述

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14、

atp perilune the landing thruster is ignited, and a propulsive landing is performed.

当到达近月点时,着陆制动发动机点火,开始动力下降阶段。

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15、

ignition start-up course calculation and ignition charge mass selection of impulse micro-thruster

微型脉冲推力器点火启动过程计算与点火药量选择

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16、

temperature drop of propellant stream in injection-tube of thruster during start process

启动过程推力器喷注管内推进剂流的温降

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17、

The advanced agile missiles possess maneuverability, agility and accurate guidance performance by adopting thruster vector control.

新型敏捷性导弹为了获得更高的机动性 、 敏捷性和更好的导引精度,许多采用推力矢量控制方案.

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18、

Experiences have been accumulated for repairing special thruster through disassembling and repairing planospiral one.

通过对平旋转推进器拆装修理,积累了对特种推进器装置修理的经验,可供参考.

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19、

Parameter distributions within the thruster and its macroscopical performance were presented.

给出了不同集气腔总压下推力器内部参数分布及其宏观性能.

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20、

Advanced agile missiles possess maneuverability, agility and precise guidance performance by adopting thruster vector control.

为了使导弹获得更高的机动性 、 敏捷性和导引精度,大多采用推力矢量控制方案.

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