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用于非接触式清除大型空间碎片物体的弱扩展楔形氙离子束的射频源。

Radio frequency source of a weakly expanding wedge-shaped xenon ion beam for contactless removal of large-sized space debris objects.

作者信息

Balashov Victor, Cherkasova Maria, Kruglov Kirill, Kudriavtsev Arseny, Masherov Pavel, Mogulkin Andrey, Obukhov Vladimir, Riaby Valentin, Svotina Victoria

机构信息

Research Institute of Applied Mechanics and Electrodynamics of the Moscow Aviation Institute (National Research University), 5 Leningrad Rd., Moscow 125080, Russia.

出版信息

Rev Sci Instrum. 2017 Aug;88(8):083304. doi: 10.1063/1.4998247.

DOI:10.1063/1.4998247
PMID:28863710
Abstract

A theoretical-experimental research has been carried out to determine the characteristics of a radio frequency (RF) ion source for the generation of a weakly expanding wedge-shaped xenon ion beam. Such ion beam geometry is of interest as a prototype of an on-board ion injector for contactless "ion shepherding" by service spacecraft to remove large space debris objects from geostationary orbits. The wedge shape of the ion beam increases its range. The device described herein comprises an inductive gas discharge chamber and a slit-type three-electrode ion extraction grid (IEG) unit. Calculations of accelerating cell geometries and ion trajectories determined the dependence of beam expansion half-angle on normalized perveance based on the measurements of the spatial distributions of the xenon plasma parameters at the IEG entrance for a xenon flow rate q ≈ 0.2 mg/s and an incident RF power P ≤ 250 W at a driving frequency f = 2 MHz. Experimental studies showed that the ion beam, circular at the IEG exit, accepted the elliptical form at the distance of 580 mm with half-angle of beam expansion across IEG slits about 2°-3° and close to 0° along them. Thus, the obtained result proved the possibility of creating a new-generation on-board ion injector that could be used in spacecrafts for removal of debris.

摘要

开展了一项理论-实验研究,以确定用于产生弱扩展楔形氙离子束的射频(RF)离子源的特性。这种离子束几何形状作为服务航天器用于非接触式“离子引导”以从地球静止轨道清除大型空间碎片物体的机载离子注入器的原型备受关注。离子束的楔形增加了其射程。本文所述的装置包括一个感应气体放电室和一个狭缝型三电极离子引出栅(IEG)单元。基于氙流量q≈0.2mg/s且驱动频率f = 2MHz时入射射频功率P≤250W的情况下,通过对IEG入口处氙等离子体参数空间分布的测量,对加速单元几何形状和离子轨迹进行计算,确定了束扩展半角对归一化导流系数的依赖性。实验研究表明,在IEG出口处呈圆形的离子束,在580mm距离处呈椭圆形,其在IEG狭缝方向上的束扩展半角约为2° - 3°,沿狭缝方向接近0°。因此,所获得的结果证明了制造可用于航天器清除碎片的新一代机载离子注入器的可能性。

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