DocumentCode :
2272294
Title :
Modeling of discharge-triggered electric field redistribution on the interior components of a satellite
Author :
Varga, L. ; Horvath, E.B. ; Haslip, D.S.
Author_Institution :
Defence Res. Establ., Ottawa, Ont., Canada
fYear :
1999
fDate :
1999
Firstpage :
39
Lastpage :
43
Abstract :
This work examines an electrostatic charging/discharging cycle of a populated circuit board inside an equipment housing of a satellite at GEO. Component potentials and electric field strengths are examined before and after a structure ground discharge event. Field reversal after the discharge suggests that favourable conditions exist for charge dissipation from the internal dielectrics at this point in time. Electric field strength dependent, this can be either spontaneous or drift related. This work was realized using a tool of two components. The charging cycle is calculated using a modified ITS-ACCEPT code. The resulting charge distribution is used as input to a 3D Poisson equation solver
Keywords :
Poisson equation; artificial satellites; electric fields; electrostatic discharge; space vehicle electronics; spacecraft charging; GEO satellite; ITS-ACCEPT code; Poisson equation; charge distribution; circuit board; dielectric component; electric field; electric potential; electrostatic charging; electrostatic discharging; equipment housing; ground discharge; Dielectric measurements; Electric potential; Electrons; Electrostatics; Plasmas; Poisson equations; Printed circuits; Satellites; Surface discharges; Telemetry;
fLanguage :
English
Publisher :
ieee
Conference_Titel :
Radiation and Its Effects on Components and Systems, 1999. RADECS 99. 1999 Fifth European Conference on
Conference_Location :
Fontevraud
Print_ISBN :
0-7803-5726-4
Type :
conf
DOI :
10.1109/RADECS.1999.858542
Filename :
858542
Link To Document :
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