An ion thruster test for NASA's Deep Space 1.
对于美国宇航局的离子推进器测试深空1号。
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。
This paper researches the manufacture technology of a new type sheathed heating material, which was used in ion thruster cathode heater.
研究了一种用于电火箭的新型铠装阴极加热器材料的性能与制造技术。
The ion energy distribution in the plasma exhaust plume of a hall thruster is important to evaluate the influence of the hall thruster plume and optimize the thruster position on the spacecraft.
霍尔推力器羽流中的离子能量分布情况对于评估推力器羽流影响，优化推力器在航天器上的布局具有重要意义。
Retarding potential analyzer (RPA) had been used to measure the ion energy distribution at a certain location downstream of the low-power hall thruster at various status.
本文使用阻滞势分析器对霍尔推力器羽流的离子能量分布进行了实验研究，获得了推力器在不同工况下羽流场中关注位置的离子能量分布状况。
As a result, they have discovered "ionic liquid ion sources" which are the core elements of the mini-thruster.
结果，他们发现“离子性液体离子源”是迷你推力器的核心元素。
As a result, they have discovered "ionic liquid ion sources" which are the core elements of the mini-thruster.
结果，他们发现“离子性液体离子源”是迷你推力器的核心元素。
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