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Azimuthal velocity measurement in the ion beam of a gridded ion thruster using laserinduced fluorescence spectroscopy

机译:使用激光致荧光光谱法在网状离子推进器的离子束中的方位角速度测量

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This paper presents the first laboratory-based study to measure the azimuthal velocities of ions in the beam of a gridded ion thruster. Through the operation of gridded ion thrusters in space, it has been confirmed that these thrusters cause an unexpected roll torque about the ion beam axis. To reveal the physical mechanism that produces this torque, laser-induced fluorescence spectroscopy has been applied to a microwave ion thruster that was installed in Japanese asteroid probes. This technique can be used to measure the azimuthal velocity by estimating the Doppler shift of the Xe II 5p~4(~3P_2)6p ~2[3] ~05/2 to Xe II 5p~4(~3P_2)6s ~2[2] 3/2 transition at 834.659 nm. The measurement was conducted without a neutralizer cathode to avoid the possibility of the cathode affecting the trajectory of the ion beam. The measured velocity functions are the sum of the spectra of the high velocity beam ions and those of charge exchange ions. By deconvolving these spectra, the azimuthal velocities were successfully measured and were found to range from -700 to 620 m s~(-1) with an accuracy of ±25%. The measured azimuthal velocity profile was accurately reproduced by the simulated velocity profile obtained using a model, which includes the effects of the maximum possible misalignment of the accelerator grid with respect to the screen grid and the Lorentz force produced by the magnetic field leaked from the discharge chamber. A roll torque of 0.5 ± 0.1 μN m about the thrust axis was calculated from the velocity profile, which is lower than that reported in flight data, but additional mechanisms are suggested to explain this discrepancy.
机译:本文介绍了基于实验室的基于实验室的研究,以测量包装离子推进器的束中离子的方位角速度。通过在空间中的包装离子推进器的操作,已经证实这些推进器导致离子束轴线的意外辊扭矩。为了揭示产生这种扭矩的物理机制,激光诱导的荧光光谱已经应用于在日本小行星探针中安装的微波离子推进器。该技术可用于通过估计XE II 5P〜4(〜3P_2)6p〜2 [3]〜05/2至XE II 5P〜4(〜3P_2)6S〜2的多普勒偏移来测量方位角速度2] 3/2过渡在834.659 nm。在没有中和剂阴极的情况下进行测量以避免阴极影响离子束的轨迹的可能性。测量的速度函数是高速光束离子的光谱和电荷交换离子的总和。通过解构这些光谱,成功测量方位角速度,并发现从-700至620 m S〜(-1)的范围为±25%。通过使用模型获得的模拟速度分布精确地再现测量的方位角速度分布,其包括通过从放电泄漏的磁场产生的屏幕网格和洛伦兹力的最大可能未对准的效果腔室。从飞行数据中报告的速度分布计算绕止推轴的辊扭矩0.5±0.1μNm的辊扭矩,但建议额外的机制来解释这种差异。

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