Charging Behavior of the H-II Transfer Vehicle by Active Electron Emission

Improved Determination of Plasma Density Based on Spacecraft Potential of the Magnetospheric Multiscale Mission under Active Potential Control

AMBER, The French Plasma Monitor onboard JASON3

High Voltage Experiment Mission Results of HORYU-IV

Photoelectron Emission Current In-Situ Measurement of Space Material in Low Earth Orbit

Correlations of Volatile Space Charging Environments with Aerospace Mechanism Friction Anomalies

P-B-1: The Research of Small Space Debris Impact Inducing Discharge on High Voltage

P-B-2: Laboratory Investigations of Electrostatic Discharge on Insulating Materials in Dusty Plasma

P-B-3: Materials Charging Investigations for Solar Orbiter

P-B-4: Electrostatic Discharges from Conductive Thermal Coatings

P-B-5: Plasma Plume Interaction with Chamber Walls during On ground Experiments: SPIS-EP Simulations and Comparison with Experiments

P-B-6: Wireless Antenna Detection of Electrostatic Discharge Events

P-B-7: Surface Potential Measurement of Coverglass using Electron Beam and Ultraviolet as Charging Method

P-B-8: 3D Printed Molybdenum for Grids and Keeper Electrodes in Ion Thruster

P-B-9*: Hybrid Fluid-Particle Plasma Modeling of a Radio-Frequency Gridded Ion Thruster

P-B-10: Model and Experimental Validation of Spacecraft-thruster Interactions for Electric Propulsion Thruster Plumes

P-B-11: Effect of Periodic Attitude Libration on Long-term Orbital Dynamics of the Electrodynamic Tether System

P-B-12: Measurements of Backflow Ions from Ion Thruster for Evaluation of Surface Erosion on HAYABUSA2

P-B-13: Energy Measurement of Backflow Ions from Ion Thruster for Estimation of Erosion Rate on HAYABUSA2 Surface Material

P-B-14: Current Measurement of Backflow Ions from Ion Thruster for Estimation of Erosion Rate on HAYABUSA2 Surface Material

P-B-15: Plume Potential Analysis for Ion Thruster Varying Spacecraft Potential by a Three-dimensional Electrostatic Full Particle Code

P-B-16: Testing and Simulation of the µCAT Plasma Plume

P-B-17*: Effects of the Two-grid Optics on a Mini Gridded Helicon Ion Thruster

P-B-18: Design and Experiment of Hollow-Cathode Plasma Contactor by a Kind of Criterion

P-B-19: Instability of Potential Oscillations for Different Type and Current Hollow Cathode

P-B-20: Electron Current Measurement of Electrodynamic Tether with Eliminating Current Collection at Tether Edge

P-B-21: Prototype Design of Surface Arc Thruster

P-B-22: Analytic Expressions of Current Collection Behavior for a Cuboid Spacecraft in a Drifting Plasma and Preparing for Tethered CubeSat Experiments, the MiTEE Mission

P-B-23: Development of Vacuum Arc Thruster with Plasma Interaction Ignition for Nanosatellite

P-B-24: Particle Simulation on the Electromagnetic Environment of Ion Thruster Beam Neutralization

P-B-25: Plasma Particle Simulation of ECR Plasma Generation in Air Breathing Ion Engine (ABIE)

P-B-26: Electrostatic Dust Transportation due to Secondary Electron Emission and Surface Electric Field above the Lunar Terminator

P-B-27: (Withdrawn by the Authors)

P-B-28*: Laboratory Investigations of Dusty Spacesuit Arcing in Plasma

P-B-29*: Numerical Simulation of Charged Dust Transport around Irregularly Shaped Small Asteroids

P-B-30: Ground Testing and Modelling of Dust Charging and Adhesion

P-B-31: Techniques for Evaluating the Risk of Internal Space Charging on Long Time-Scale Orbits

P-B-32: Hybrid PIC Code for Active Shielding Demonstration Inspired from Magneto Plasma Sail

P-B-33: Comparison of Magnetospheric Magnetic Field Variations at Quasi-Zenith Orbit Based on Michibiki Observation and REPPU Global MHD Simulation

P-B-34: Plume Structure Study of Cathodic Plasma Contactor

P-B-35: Transformation of Energy and Charge Deposition Profiles between Normally Incident and Isotropically Incident Electrons for Various Materials

P-B-36: Electron Range Computational Tool for Arbitrary Materials over a Wide Energy Range

Hybrid Fluid-Particle Plasma Modeling of a Radio-Frequency Gridded Ion Thruster (P-B-9)

Numerical Simulation of Charged Dust Transport around Irregularly Shaped Small Asteroids (P-B-29)

Laboratory Investigations of Dusty Spacesuit Arcing in Plasma (P-B-28)

Effect of Damage Accumulation in Microcircuits under the Series of IESD (P-A-31)

On the Use of a Detailed Electron Emission Model for Spacecraft Charging at Low Energy (P-C-17)

Remote Sensing of Spacecraft Electrostatic Potential using Secondary Electrons (P-C-28)

Simulations of the Rosetta Spacecraft Interaction with Comet Plasma (P-C-4)

Effects of the Two-grid Optics on a Mini Gridded Helicon Ion Thruster (P-B-17)

Arc Plasma Propagation and Arc Current Profiles

Electrostatic Testing of Multilayer Insulation for In-Space Cryogenic Vehicles

Test Set-up Review for Arcing Test on New Solar Array Generation

Transient Characteristics of Charging Effects due to E-beam Irradiation: A Method of Charging Balance Mode

Simulation of the Effect of Time-Dependent Electron Environment on the Internal Charging Dynamic using SPIS-IC

Spacecraft Inner Charging Simulation of the Electronics Devices Plastic Cases

Validation of Internal Charging Tools with REEF data

Electric-Orbit-Raising Induced Deep Charging Requirement and Analysis of External Satellite Harness with Shields

Long Term Charge Buildup and Dissipation in Spacecraft Materials