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Experiment/Payload OverviewPlasma Electron Gun Payload (PLEGPAY) will validate the plasma contactor as an active device on the International Space Station for the prevention/control of electrostatic charging phenomena on large space structures orbiting at low Earth orbit.
Principal InvestigatorInformation Pending
Payload DeveloperInformation Pending
Sponsoring AgencyEuropean Space Agency (ESA)
Expeditions Assigned|16|17|18|19|20|
Previous ISS MissionsInformation Pending
The scientific objective of PLEGPAY experiment is the study of the spacecraft/space environment interactions in LEO, with reference to electrostatic charging/discharging phenomena. The spacecraft community is very interested to understand the mechanisms for electrostatic charge accumulation, which often produce uncontrollable discharge events, thereby adversely affecting the functioning of spacecraft electronic systems. Among the existing active methods to mitigate charging effects, the hollow cathode plasma contactor (an electric propulsion spin-off technology) has proved itself to be the most effective technology. A hollow cathode plasma contactor, as applied in PLEGPAY, and used to control the spacecraft charging in order to safeguard the spacecraft operation, could, in the near future, become a standard facility at disposal of the commercial and scientific satellites and space station/infrastructures.
Information Pending
Earth ApplicationsInformation Pending
Information Pending
Operational ProtocolsInformation Pending
Information Pending