Development and characterization of the ECLIPS space environments simulation facility
Touchless Potential Sensing of Differentially Charged Spacecraft Using X-Rays
Coupled Spacecraft Charging Due to Continuous Electron Beam Emission and Impact
Impact of Electrostatic Perturbations on Proximity Operations in High Earth Orbits
Using Plasma-Induced X-Ray Emission to Estimate Electrostatic Potentials on Nearby Space Objects
Touchless Potential Sensing of Differentially Charged Spacecraft Using Secondary Electrons