论文标题
Rosetta航天器的充电模型
A charging model for the Rosetta spacecraft
论文作者
论文摘要
语境。航天器VS的静电电势对于原位等离子体测量的能力很重要。在大多数彗星任务中,Rosetta被发现负责负责,甚至在更密集的等离子会中。目标。我们的目标是研究负VS与电子密度和温度的相关性,并了解观察到的相关性的物理。方法。我们应用了VS,电子温度和电子密度的完整任务比较统计,以建立对冷和温暖的血浆密度和电子温度的依赖。我们还使用了航天器 - 血浆相互作用系统(SPI)模拟和分析真空模型来研究覆盖太阳阵列表面一部分的正相偏置元素是否可以解释观察到的相关性。结果。在这里,发现VS更多地取决于电子密度,尤其是电子的冷部分,而对电子温度的高度比热(彗星)电离层电子的高通量所预期的要少。这种行为是由与数值模拟一致的分析模型复制的。结论。罗塞塔(Rosetta)主要是由太阳能电池板前侧边界上的积极偏置元素驱动的,因为这些元素可以有效地收集冷等离子体电子。面板前侧分布在其他地方的偏置元件在收集电子(光电子)以外的电子(光电子)外的效率较低。为了避免大量充电,未来的航天器可能会最大程度地减少裸露偏置导体的面积或使用正地面电力系统。
Context. The electrostatic potential of a spacecraft, VS, is important for the capabilities of in situ plasma measurements. Rosetta has been found to be negatively charged during most of the comet mission and even more so in denser plasmas. Aims. Our goal is to investigate how the negative VS correlates with electron density and temperature and to understand the physics of the observed correlation. Methods. We applied full mission comparative statistics of VS, electron temperature, and electron density to establish VS dependence on cold and warm plasma density and electron temperature. We also used Spacecraft-Plasma Interaction System (SPIS) simulations and an analytical vacuum model to investigate if positively biased elements covering a fraction of the solar array surface can explain the observed correlations. Results. Here, the VS was found to depend more on electron density, particularly with regard to the cold part of the electrons, and less on electron temperature than was expected for the high flux of thermal (cometary) ionospheric electrons. This behaviour was reproduced by an analytical model which is consistent with numerical simulations. Conclusions. Rosetta is negatively driven mainly by positively biased elements on the borders of the front side of the solar panels as these can efficiently collect cold plasma electrons. Biased elements distributed elsewhere on the front side of the panels are less efficient at collecting electrons apart from locally produced electrons (photoelectrons). To avoid significant charging, future spacecraft may minimise the area of exposed bias conductors or use a positive ground power system.