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Low Earth Orbit Plasma Wake Shaping and Applications to On-Orbit Proximity Operations

机译:低地球轨道等离子体唤醒成形及其在近距离操作中的应用

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A parametric investigation of plasma wake geometry is conducted to determine the applicability of Coulomb actuation to resident space objects (RSOs) in low earth orbit (LEO). The use of Coulomb forces could provide a touchless means to achieve the relative position and attitude adjustments between close-proximity objects on orbit. Theoretical models developed for techniques in the geosynchronous earth orbit (GEO) regime indicate that Coulomb actuation could facilitate on-orbit proximity operations in a highly fuel- and power-efficient manner. In LEO, however, only the plasma parameters in the wakes behind orbiting objects are a promising region for Coulomb actuation applications. These physical phenomena investigated by the charging hazards and wake studies (CHAWS), space experiments with particle accelerators (SEPAC), and other on-orbit experiments exhibit substantially decreased plasma density relative to the surroundings. This investigation considers the wake which forms behind objects of various potentials and cross-sectional areas, particularly focusing on methods of enhancing the wake with negligible changes in the objects' area, and therefore their mass. Experimental results are presented and compared with previous theoretical, numerical, and experimental works. The size of a wake formed by an uncharged object is shown to depend on its cross-sectional area. However, the same object charged to a positive potential generates a substantially larger wake. Additional experimental results indicate that a positively charged, sparse structure with similar dimensions, but significantly less cross-sectional area forms a wake similar to the previous, solid object charged to the same level. This indicates that a large wake can be generated without significantly increasing the mass or area-dependent perturbations such as the drag and the solar radiation pressure. These results increase the applicability of Coulomb actuation in LEO by enhancing the region in which the technique is feasible.
机译:进行了等离子体尾流几何形状的参数研究,以确定库仑驱动对低地球轨道(LEO)中的常驻空间物体(RSO)的适用性。库仑力的使用可以提供一种非接触方式,以实现在轨道上接近物体之间的相对位置和姿态调整。为地球同步地球轨道(GEO)领域的技术开发的理论模型表明,库仑驱动可以以高燃料和功率效率的方式促进在轨近距离操作。然而,在LEO中,只有绕天轨道后的尾流中的等离子体参数才是库仑驱动应用的有希望的领域。这些通过充电危害和唤醒研究(CHAWS),使用粒子加速器进行的空间实验(SEPAC)以及其他在轨实验研究的物理现象显示出相对于周围环境而言,等离子体密度大大降低了。这项研究考虑了在各种电位和横截面积的物体后面形成的尾流,特别是侧重于通过在物体区域及其质量的变化可忽略不计的情况下增强尾流的方法。介绍了实验结果,并将其与以前的理论,数值和实验工作进行了比较。由不带电物体形成的尾流的大小显示为取决于其横截面积。但是,带正电的同一物体会产生明显更大的唤醒。其他实验结果表明,带正电的稀疏结构具有相似的尺寸,但截面积却显着减小,形成的尾流类似于以前的带电至相同水平的固体物体。这表明可以在不显着增加质量或与面积有关的扰动(例如阻力和太阳辐射压力)的情况下产生较大的尾流。这些结果通过扩大该技术可行的区域,增加了库仑驱动在LEO中的适用性。

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