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Electron irradiation tests on European meteorological satelliteThe observation of in orbit anomalies on Meteosat resulted in a test being performed to establish the charging and discharging characteristics of a flight configured engineering model when irradiated with electrons. Surface potentials were measured together with discharge rates and amplitudes. Results indicate that a large number of discharges are possible on the satellite whether or not the external surfaces are grounded. Initial measurements show that there are very high potential gradients around the satellite which obviously contribute largely to the discharging behavior. The time constant for charging is very small, indicating also that equilibrium conditions are achieved very quickly as the local ambient changes in orbit. A.R.H.
Document ID
19820006393
Acquisition Source
Legacy CDMS
Document Type
Conference Paper
Authors
Reddy, J.
(European Space Agency Paris, France)
Date Acquired
August 10, 2013
Publication Date
October 1, 1980
Publication Information
Publication: NASA. Lewis Research Center Spacecraft Charging Technol., 1980
Subject Category
Spacecraft Design, Testing And Performance
Accession Number
82N14266
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.

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