The 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.
Electron irradiation tests on European meteorological satellite
1980-10-01
Conference paper
No indication
English
The European meteorological satellite programme
SLUB | 1998
|Geosynchronous meteorological satellite.
AIAA | 1969
|Geosynchronous meteorological satellite
NTRS | 1970
|Geosynchronous meteorological satellite
AIAA | 1968
|