4.3 Article

Dependence of Solar Cell ESD Voltage Threshold on Cover Glass Secondary Emission Properties

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IEEE-INST ELECTRICAL ELECTRONICS ENGINEERS INC
DOI: 10.1109/TPS.2023.3250712

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Electrostatic discharges; Numerical models; Glass; Electric potential; Surface charging; Dielectrics; Conductivity; Electrostatic discharge (ESD); numerical simulation; secondary electron yield; spacecraft charging

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Spacecraft can be charged when they come into contact with charged particles in space. The charging is influenced by the surface materials and their exposure to space, resulting in different charging levels for different parts of the spacecraft. The charging on solar panels is especially important due to the polarized elements and small distances between them, leading to strong electric fields and electrostatic discharges (ESDs). This article focuses on controlling the onset of ESDs by studying the impact of cover glass secondary emission properties on the voltage threshold of solar cell ESDs. Numerical simulations using the spacecraft plasma interaction software (SPIS)-ESD software are conducted, as practical experimental studies are not feasible due to the natural variability of physical samples and the lack of materials with controlled characteristics.
Spacecraft interacts with the charged particles of the space environment, leading to their electrostatic charging. This charging depends on the surface materials and their exposure to space. Thus, it is different for different parts of the spacecraft. This differential charging is particularly important on solar panels, which are composed of various polarized elements juxtaposed over small distances. This leads to strong electric fields ultimately leading to electrostatic discharges (ESDs), themselves being the onset of destructive secondary arcs. Hence, controlling the onset of ESDs is a key factor to prevent damages on spacecraft. Two ways are generally envisioned to act on the ESD onset: the geometry of the solar cells and the material electrostatic properties. In this article, the control of the ESD onset is tackled through the study of the effects of the cover glass secondary emission properties on the voltage threshold of solar cell ESDs. This study is conducted numerically with the spacecraft plasma interaction software (SPIS)-ESD software, as the natural variability of physical samples and the impossibility to have materials with controlled characteristics render the experimental study unpractical, if even feasible.

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