IEEE Transactions on Nuclear Science · 2004 · 12 citations · 7 references
Natural SciencesAerospace EngineeringPhysicsElectrochemistryPlasma PhysicsSpacecraft DesignCharged Particle DetectionCharging SystemsSurface ChargeCharge DetectionSolar Cycle EffectsSolar Cycle VariabilitySpace Charge MeasurementSpacecraft ChargingSurface ChargingSurface Charging MechanismsSurface Potential
An analysis of differential charging between dielectric surface materials and the frame of a DSCS-III geosynchronous spacecraft is presented. Charging levels measured by surface potential monitors (SPMs) covered with samples of Kapton and Astroquartz have been recorded for one half of a solar cycle. Both seasonal and solar cycle effects are seen in the daily peak levels of the SPM voltages, with local maxima occurring near the equinoxes and a general trend increasing as solar max is approached. Charge neutralization by an onboard Xe plasma contactor was demonstrated to be effective throughout the mission, with a mean voltage reduction of 86% for Astroquartz and 74% for Kapton. Though a statistical analysis shows a general correlation between the fluence of charging electrons with SPM voltages, the event-specific correlation contains enough variance to cast doubt on the usefulness of an electron sensor as a differential charging alarm. We have found that a Kapton-covered SPM may be better suited than an electron sensor as a differential charging alarm.
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