Coupled Spacecraft Charging Due to Continuous Electron Beam Emission and Impact
Charged aerodynamics: Ionospheric plasma drag on objects in low-Earth orbit
Space Environment Effects on the Electron Yields of Thermal Control Coatings
Touchless Potential Sensing of Differentially Charged Spacecraft Using X-Rays
Electrostatic Discharge Tests of Carbon Composite Materials with Conductive Resin
Using Plasma-Induced X-Ray Emission to Estimate Electrostatic Potentials on Nearby Space Objects
Touchless Potential Sensing of Differentially Charged Spacecraft Using Secondary Electrons
Electron-Based Touchless Potential Sensing of Shape Primitives and Differentially-Charged Spacecraft
Development and characterization of the ECLIPS space environments simulation facility
Simulation and Uncertainty Quantification of Electron Beams in Active Spacecraft Charging Scenarios
Impact of Electrostatic Perturbations on Proximity Operations in High Earth Orbits
Electrostatic Levitation on Atmosphere-Less Planetary Bodies with Ionic-Liquid Ion Sources
Multicomponent Plasma Expansion Model for Arc Discharges on Large-Area Solar Arrays
NASA Air Force Spacecraft Charging Analyzer Program Confirmation of GPS Arcing
Electrostatic Tractor Analysis Using a Measured Flux Model
Rapid Modeling of Electrostatic Forces and Torques Considering Dielectrics
Immersed Finite Element Particle-in-Cell Simulations of Plasma Charging at the Lunar Terminator