Understanding the Potential Dangers of Spacecraft
Engineering teams investigating the failure identified charging by high energy auroral electrons followed by an electrostatic discharge
The status of the ionospheric space weather, in particular solar activity/storms affects the density, in particular local density that can increase charging and currents. Motional EMF affects ISS charging because of the size of the ISS vehicle, in particular the length of the truss.
Energetic charged particles (primarily energetic electrons), sunlight/photoemission, and secondary electron emission are the most important natural factors affecting spacecraft charging in magentospheric and cis-lunar environments beyond LEO .
The ISS spacecraft charging detection and warning process identifies possibly hazardous conditions before they occur and advises ISS management in time to activate EVA shock hazard controls as needed .
The ISS spacecraft charging environments and physical mechanisms are radically different from those encountered at higher altitudes in Earth's magnetosphere and in cis-lunar and interplanetary space. Collection of ions and electrons (current collection) modifies the ISS floating potential (FP), , , , .
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