Opening Remark by the President of Kobe University (abstract)

Spacecraft Charging Study in Japan (abstract)

USA Overview (abstract)

Present Day Status of Spacecraft Charging Investigations in Russia (abstract)

Overview of Activities Europe-wide and in France (abstract)

Status of Spacecraft Charging Study in China (abstract)

An Overview of Spacecraft Charging Research in India: Spacecraft Plasma Interaction Experiments—SPIX–III (abstract)

P-A-1*: Orbital and Storm Analysis of the Pulsed Electrostatic Tractor using Statical Flux Distributions (abstract)

P-A-2: Observations of Frame Charging by the MPS-LO Instrument on GOES-16 (abstract)

P-A-3: Updating the Europa Spacecraft Charging Environment (abstract)

P-A-4*: Low Earth Orbit Plasma Wake Shaping and Applications to On-Orbit Proximity Operations (abstract)

P-A-5: Tools for Understanding On-orbit Satellite Anomalies (abstract)

P-A-6: Statistical Study of Surface-charging Events in Aurora Region over One Solar Cycle (abstract)

P-A-7*: Development of a Real-time Risk Estimation Method of Spacecraft Surface Charging (abstract)

P-A-8: The Impact of Auroral Electron Streams on LEO Polar Satellites as a Source of Charging (abstract)

P-A-9: Statistical Analysis of Spacecraft Charging Environment in the Medium Earth Orbit (abstract)

P-A-10*: Surface Charging Analysis of the Quasi-Zenith Satellite “MICHIBIKI” (abstract)

P-A-11: Prediction of the Outer Radiation Belt Variation by Kalman Filter based on Realtime Data of the Arase Satellite and Dst Index (abstract)

P-A-12: The Development of Space Instrumentation for In-situ Measurements of the LEO Environment and Test Facilities for Induced, High-frequency Plasma Instabilities (abstract)

P-A-13: Arcing on Solar Generators by Collection of Ionospheric Plasma Currents (abstract)

P-A-14: Radiofrequency Interference from Satellite Solar Array Arcing (abstract)

P-A-15: Studying Interaction of Hot Magnetospheric Plasma with Spacecraft Solar Array Protective Coating (abstract)

P-A-16*: XPS Investigation of the Source of GPS Arc Contamination (abstract)

P-A-17*: Mission Report of a Double Langmuir Probe Onboard HORYU-IV Satellite (abstract)

P-A-18: Nanosatellite Constellation for 3D Ionosphere Mapping (abstract)

P-A-19: Result of Plasma Measurement in HTV during ISS Attached Phase (abstract)

P-A-20: LEO Charging of the PICASSO Cubesat and Simulation of the Langmuir Probes Operation (abstract)

P-A-21: Charging of geostationary satellite Electro-L2 in the Earth shadow (abstract)

P-A-22: Multi-needle Langmuir Probe Operation and Acute Probe Current Susceptibility to Spacecraft Potential (abstract)

P-A-23: Internal Charging Issues Met during Electric Orbit Raising (abstract)

P-A-24: Measurement of Internal Charge Distribution in Dielectrics under High Energy Electron Irradiation (abstract)

P-A-25: Study on Quantitative Evaluation Method for Charging Effect of Orbit Spacecraft (abstract)

P-A-26: Influence of Dielectric Charging on Microwave Discharge Process in Microwave Impedance Converter (abstract)

P-A-27: A Method of Finding Optimal Parameters of Deep Charging Environmental Indicators by Using Orbital Anomaly Data of GEO Satellite (abstract)

P-A-28: Computer Simulations and Experimental Investigation for Heterodyne Characteristics on PCB with the Increased Resistance to Electrostatic Discharges (abstract)

P-A-29: (Withdrawn by the Authors) (abstract)

P-A-30: Experimental and Numerical Characterizations of Current and Magnetic Fields Produced by Electrostatic Discharge due to Internal Charging (abstract)

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

P-A-32: Internal Charging Simulation for Satellite based on Reverse Monte Carlo Method (abstract)

P-A-33: Internal Electrostatic Discharge (iESD) Design Guidelines for Jovian Missions (abstract)

P-A-34*: Study of Internal Charging of Polymers through Numerical and Experimental Analyses - Comparison of Different Space used Numerical Tools (abstract)

P-A-35: Internal Charging Analysis of a Realistic Experiment with a Dedicated Modelling Chain (abstract)

P-A-36: Experimental Study of Deep Dielectric Discharging of Polymer under Energetic Electron Irradiation (abstract)

P-A-37: (Moved to Oral Session 12) (abstract)

P-A-38: Characteristics of Electron - Hole Pairs Generation in Fluorinated Polymer Irradiated by an Electron (abstract)

P-A-39: Analysis of Deterioration Phenomena on Fluorinated Insulating Material Irradiated by Proton and Electron (abstract)

Development of a Real-time Risk Estimation Method of Spacecraft Surface Charging (P-A-7) (abstract)

Surface Charging Analysis of the Quasi-Zenith Satellite “MICHIBIKI” (P-A-10) (abstract)

Low Earth Orbit Plasma Wake Shaping and Applications to On-Orbit Proximity Operations (P-A-4) (abstract)

Orbital and Storm Analysis of the Pulsed Electrostatic Tractor using Statical Flux Distributions (P-A-1) (abstract)

Study of Internal Charging of Polymers through Numerical and Experimental Analyses - Comparison of Different Space used Numerical Tools (P-A-34) (abstract)

An Efficient Hybrid Approach for the Reduction of Secondary Electron Yield (P-C-31) (abstract)

XPS Investigation of the Source of GPS Arc Contamination (P-A-16) (abstract)

Mission Report of a Double Langmuir Probe Onboard HORYU-IV Satellite (P-A-17) (abstract)

Suppression of Local Surface Charging on the ERG (Arase) Satellite (abstract)

GOES-R-series Radiation Belt Observations in Support of Internal Charging Alerts and Investigations (abstract)

Trapped Electron Environments of the Outer Planets (abstract)

Physical and Spectrometric Analysis of Electron-Damaged LDPE (abstract)

Evidence for Arcing on the International Space Station Solar Arrays (abstract)

The Case for GPS Arcing and High Satellite Arc Rates (abstract)

Arcing Risk due to Micrometeorite/Debris Impact on Flexible Solar Array with 100V Bus Voltage (abstract)

Semi-analytical Model of the Current Collection by the Interconnects and Cell Edges of High Voltage Solar Panels Exposed to LEO or Thruster Plume Plasma: Numerical Models and Comparison with Experimental Data (abstract)

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

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

AMBER, The French Plasma Monitor onboard JASON3 (abstract)

High Voltage Experiment Mission Results of HORYU-IV (abstract)

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

Correlations of Volatile Space Charging Environments with Aerospace Mechanism Friction Anomalies (abstract)

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

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

P-B-3: Materials Charging Investigations for Solar Orbiter (abstract)

P-B-4: Electrostatic Discharges from Conductive Thermal Coatings (abstract)

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

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

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

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

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

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

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

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

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

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

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

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

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

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

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

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

P-B-21: Prototype Design of Surface Arc Thruster (abstract)

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 (abstract)

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

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

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

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

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

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

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

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

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

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

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

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

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

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

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

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

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

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

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

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

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

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

Arc Plasma Propagation and Arc Current Profiles (abstract)

Electrostatic Testing of Multilayer Insulation for In-Space Cryogenic Vehicles (abstract)

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

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

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

Spacecraft Inner Charging Simulation of the Electronics Devices Plastic Cases (abstract)

Validation of Internal Charging Tools with REEF data (abstract)

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

Long Term Charge Buildup and Dissipation in Spacecraft Materials (abstract)

The Breakdown of the Fluid Approximation for Electrons in Mesothermal Plasma Expansion and Its Implications on Plasma Plume/Wake Models (abstract)

Coupling of a All-electric Spacecraft with its Plasma Plume and its Environment (abstract)

Development of a Three-dimensional Electrostatic Code for Hall Thruster Plume and Spacecraft Interaction Analysis (abstract)

Study on Lorentz Force Characteristics of Electrodynamic Tether System Based on Hollow Cathode (abstract)

*PLENARY TALK: The Effects of Dust Charging in Space and the Laboratory (abstract)

Numerical Modelling of the Lunar Exosphere and Lunar Lander Interactions with SPIS-DUST (abstract)

The Effect of Plasma Cloud Expansion Associated with Dust Impacts (abstract)

Modeling Surface Charging for NASA's Europa Clipper Mission (abstract)

High-fidelity Multi-Length Scale Modeling of Spacecraft Charging in GEO Orbit (abstract)

Advanced Numerical Schemes Implemented in SPIS to Improve the Accuracy of the Description of the Dense Cold and Drifting Plasma Populations (abstract)

Impact of Miniaturized Fixed-bias Multi-Needle Langmuir Probes on CubeSats (abstract)

Simulation of the Electrostatic Environment of the Magnetospheric Multiscale Mission (abstract)

Numerical Simulation of Spacecraft Charging Processes in Time-varying Plasma Environment (abstract)

P-C-1: Simulation and Analysis of the SMILE Charging using SPIS (abstract)

P-C-2: Spacecraft Surface Charging Simulation based on 3D Electrostatic PIC Model (abstract)

P-C-3: Simulations of Non-ideal Effects In Langmuir Probe Measurements (abstract)

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

P-C-5: Improvement of the Spacecraft-Plasma Interaction Software (SPIS) with a New Versatile Architecture and Enhanced Modeling Capabilities for Electric Propulsion (abstract)

P-C-6: (Moved to Oral Session 15) (abstract)

P-C-7: Wake Formation behind Small Satellites (abstract)

P-C-8: Differential Charging Estimation of Spacecraft in Single and Double Maxwellian Plasma Environment (abstract)

P-C-9: Current Status of MUSCAT (Multi-Utility Spacecraft Charging analysis tools) (abstract)

P-C-10: Particle Simulation Analysis of Spacecraft Charging Processes in Plasma Wave Environment (abstract)

P-C-11: Numerical Study on the Plasma Disturbance an Charging Processes by Booms of an Ionospheric Rocket (abstract)

P-C-12: Numerical Study on Plasma Disturbance near a Low-Earth Orbit Satellite (abstract)

P-C-13: Charging Characteristics of Electron Irradiated Polyimide Film under Cryogenic Temperature (abstract)

P-C-14: The Secondary Electron Emission Properties and the Influence on Charging Potentials (abstract)

P-C-15: A Consideration of Degradation of Polymeric Materials in Sub-Low Earth Orbit Space Environment (abstract)

P-C-16: Development of a Pulsed Supersonic Valve Aimed for Martian Atmospheric Simulation (abstract)

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

P-C-18: Modification of Charge Body Migration in LDPE as a Result of Electron Radiation Exposure. (abstract)

P-C-19: Effect of Plume Interaction with Spacecraft Materials on Electron Emission Properties and Electrical Characteristics (abstract)

P-C-20: Dielectric Charging Mechanisms Involved in the Non-typical Electron Emission Yield Observed for Thin Dielectric Layers (abstract)

P-C-21: Secondary Electron Yield Measurements of Carbon Nanotube Forests: Dependence on Morphology and Substrate (abstract)

P-C-22: Charging Analysis with Changing the Satellite Surface Material Property due to Space Environment (abstract)

P-C-23: Construction of Measurement System for Carrier Mobility in Insulating Materials for Spacecraft (abstract)

P-C-24: Measurements of the Intrinsic Electron Yield of Highly Insulating Materials (abstract)

P-C-25: Parameterization of Secondary and Backscattered Electron Yields for Spacecraft Charging (abstract)

P-C-26: Electron Yield of Carbon-Composite Nanodielectric Material (abstract)

P-C-27: Method for Touchless Determination of Electrostatic Potential and Material Composition for Spacecraft (abstract)

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

P-C-29: Detailed Charging Analysis of Exposed KAPTON in GSAT-19 (abstract)

P-C-30: Concerning of the Spacecraft Charging for Space Debris Removal and Orbital Services (abstract)

P-C-31*: An Efficient Hybrid Approach for the Reduction of Secondary Electron Yield (abstract)

P-C-32: Dielectric Barriers for Arc Mitigation (abstract)

P-C-33: Enabling Electron Beam Use in Tenuous Space Plasmas using Plasma Contactors: the Ion Emission Model (abstract)

P-C-34: Dynamic Attenuation of Secondary Electrons Emission Yield of Fluorinated Polyimide Films (abstract)

P-C-35: Significance of Shielding Kernel Selection for Spacecraft Charging Assessments (abstract)

P-C-36: Improved Spacecraft Charging Roadmaps Developed to Support User Community Needs (abstract)

P-C-37: Testing Materials under Electron Spectra Representative of GEO Worst-case Environments for Surface Charging (abstract)

The Suppression of Spacecraft Charging based on Nanographene Composite (abstract)

Worst-case Surface Charging: On the Importance of Measuring the Electron Emission Yield under Representative Environmental Conditions (abstract)

Electrical Ageing of Polymers under Space Radiation Environment (abstract)

Analysis of Charge Accumulation Phenomena by Physicochemical Analysis for Fluorinated Polymer Films Irradiated by Proton (abstract)

Radiation-induced Conductivity in Kapton-like Polymers Featuring Conductivity Rising with Accumulating Dose (abstract)

Conductivity of Thermal Control White Paints as a Function of Temperature and Surface Voltage (abstract)

Time Evolved Constant Voltage Conductivity Measurements of Common Spaceborn Polymeric Materials (abstract)

Spacecraft Charging Material Properties Database (abstract)

Quantifying Spacecraft Specific Surface-Charging Risk in Geostationary Orbit (abstract)

Preventing Electrostatic Discharge in the Mars 2020 PIXL X-Ray Tube (abstract)

Study on a Method of Stabilizing the Electron Emission of ELFs-charm (abstract)

The Defending Film of LEO Spacecraft High-voltage Solar Array Charging Effect (abstract)

Guidelines for Space Weather Research and Operation discussed in Space Weather Expert Group (SWEG) in UNCOPUOS /LTS WG (abstract)

Spacecraft Potential Estimation in Worst Case Environment (abstract)

Poster Award Presentation (abstract)

Closing Remark by the Chair of SCTC2018 (abstract)