首页> 外文期刊>Nuclear Instruments & Methods in Physics Research. B, Beam Interactions with Materials and Atoms >Hypervelocity dust impact craters on photovoltaic devices imaged by ion beam induced charge
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Hypervelocity dust impact craters on photovoltaic devices imaged by ion beam induced charge

机译:超高速尘埃撞击离子束感应电荷成像的光伏器件上的火山口

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Hypervelocity dust has a speed of greater than 5 km/s and is a significant problem for equipment deployed in space such as satellites because of impacts that damage vulnerable components. Photovoltaic (PV) arrays are especially vulnerable because of their large surface area and the performance can be degraded owing to the disruption of the structure of the junction in the cells making up the array. Satellite PV arrays returned to Earth after service in orbit reveal a large number of craters larger than 5 μm in diameter arising from hypervelocity dust impacts. Extensive prior work has been done on the analysis of the morphology of craters in PV cells to understand the origin of the micrometeoroid that caused the crater and to study the corresponding mechanical damage to the structure of the cell. Generally, about half the craters arise from natural micrometeoroids, about one third from artificial Al-rich debris, probably from solid rocket exhausts, and the remainder from miscellaneous sources both known and unknown. However to date there has not been a microscopic study of the degradation of the electrical characteristics of PV cells exposed to hypervelocity dust impacts. Here we present an ion beam induced charge (IBIC) pilot study by a 2 MeV He microbeam of craters induced on a Hamamatsu PIN diode exposed to artificial hypervelocity Al dust from a dust accelerator. Numerous 5-30 μm diameter craters were identified and the charge collection efficiency of the crater and surrounds mapped with IBIC with bias voltages between 0 and 20 V. At highest bias, it was found the efficiency of the crater had been degraded by about 20% compared to the surrounding material. The speed distribution achieved in the Al dust accelerator was peaked at about 4 km/s compared to 11-68 km/s for dust encountered in low Earth orbit. We are able to extrapolate the charge collection efficiency degradation rate of unbiased cells in space based on our current measurements and the differences in the structure of the targets.
机译:超高速尘埃的速度大于5 km / s,这对部署在卫星等太空中的设备来说是一个重大问题,因为它会损坏易损部件。光伏(PV)阵列由于其大的表面积而特别容易受到损害,并且由于构成该阵列的单元中的结的结构的破坏而可能降低性能。在轨道服役后返回地球的卫星光伏阵列显示,由于超高速尘埃撞击,产生了许多直径大于5μm的陨石坑。在分析PV电池中的陨石坑的形态方面已经进行了广泛的研究,以了解引起陨石坑的微流线型的起源,并研究对电池结构的相应机械损伤。通常,陨石坑的大约一半来自天然的微流星体,大约三分之一来自人造的富含Al的碎片,可能来自固体火箭废气,其余的来自已知和未知的其他来源。然而,迄今为止,尚未有微观研究暴露于超高速尘埃冲击的PV电池的电特性的下降。在这里,我们介绍了由2 MeV He微束束的离子束感应电荷(IBIC)初步研究,该束微束在暴露于来自粉尘加速器的人工超高速Al粉尘的Hamamatsu PIN二极管上诱发。鉴定出许多直径为5-30μm的陨石坑,并使用偏置电压在0至20 V之间的IBIC绘制了陨石坑和周围环境的电荷收集效率。在最高偏压下,发现陨石坑的效率下降了约20%与周围的材料相比。铝粉尘加速器中达到的速度分布峰值约为4 km / s,而低地球轨道遇到的粉尘为11-68 km / s。我们能够根据当前的测量结果和靶标结构的差异,推断空间中无偏电池的电荷收集效率降低率。

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