SCTC2018: THE 15TH SPACECRAFT CHARGING TECHNOLOGY CONFERENCE

This page contains an index consisting of author-provided keywords.

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-charging effect	P-C-20: Dielectric Charging Mechanisms Involved in the Non-typical Electron Emission Yield Observed for Thin Dielectric Layers
-electron emission	P-C-20: Dielectric Charging Mechanisms Involved in the Non-typical Electron Emission Yield Observed for Thin Dielectric Layers
-electron emission model	P-C-20: Dielectric Charging Mechanisms Involved in the Non-typical Electron Emission Yield Observed for Thin Dielectric Layers
3
3D electrostatic PIC	P-C-2: Spacecraft Surface Charging Simulation based on 3D Electrostatic PIC Model
3D simulation	P-A-30: Experimental and Numerical Characterizations of Current and Magnetic Fields Produced by Electrostatic Discharge due to Internal Charging
A
ABIE	P-B-25: Plasma Particle Simulation of ECR Plasma Generation in Air Breathing Ion Engine (ABIE)
Absolute Voltage	AMBER, The French Plasma Monitor onboard JASON3
Advanced numerical schemes	Advanced Numerical Schemes Implemented in SPIS to Improve the Accuracy of the Description of the Dense Cold and Drifting Plasma Populations
Ageing	Electrical Ageing of Polymers under Space Radiation Environment
Agencies	Overview of Activities Europe-wide and in France
air breathing ion engine	P-B-25: Plasma Particle Simulation of ECR Plasma Generation in Air Breathing Ion Engine (ABIE)
Amber	AMBER, The French Plasma Monitor onboard JASON3
Analysis tools	P-C-9: Current Status of MUSCAT (Multi-Utility Spacecraft Charging analysis tools)
Angular distribution	P-C-17*: On the Use of a Detailed Electron Emission Model for Spacecraft Charging at Low Energy
Arase satellite	P-A-11: Prediction of the Outer Radiation Belt Variation by Kalman Filter based on Realtime Data of the Arase Satellite and Dst Index
Arc Detection by Earthbound Reconnaissance	USA Overview
Arc Plasma Propagation	Arc Plasma Propagation and Arc Current Profiles
Arc-Plasma Expansion	USA Overview
arcing	Preventing Electrostatic Discharge in the Mars 2020 PIXL X-Ray Tube P-C-32: Dielectric Barriers for Arc Mitigation Test Set-up Review for Arcing Test on New Solar Array Generation P-B-6: Wireless Antenna Detection of Electrostatic Discharge Events P-A-13: Arcing on Solar Generators by Collection of Ionospheric Plasma Currents Evidence for Arcing on the International Space Station Solar Arrays P-A-16*: XPS Investigation of the Source of GPS Arc Contamination
arcing risk	Arcing Risk due to Micrometeorite/Debris Impact on Flexible Solar Array with 100V Bus Voltage
asteroid charging	P-B-29*: Numerical Simulation of Charged Dust Transport around Irregularly Shaped Small Asteroids
asteroid-dust-plasma interaction	P-B-29*: Numerical Simulation of Charged Dust Transport around Irregularly Shaped Small Asteroids
atomic oxygen	P-C-15: A Consideration of Degradation of Polymeric Materials in Sub-Low Earth Orbit Space Environment P-C-16: Development of a Pulsed Supersonic Valve Aimed for Martian Atmospheric Simulation
Attitude Libration	P-B-11: Effect of Periodic Attitude Libration on Long-term Orbital Dynamics of the Electrodynamic Tether System
aurora	P-A-20: LEO Charging of the PICASSO Cubesat and Simulation of the Langmuir Probes Operation
Auroral electron	P-C-30: Concerning of the Spacecraft Charging for Space Debris Removal and Orbital Services
B
Back-scattered Electron Yield	P-C-8: Differential Charging Estimation of Spacecraft in Single and Double Maxwellian Plasma Environment
Backflow of propellant ions	P-B-12: Measurements of Backflow Ions from Ion Thruster for Evaluation of Surface Erosion on HAYABUSA2
ball bearings	Correlations of Volatile Space Charging Environments with Aerospace Mechanism Friction Anomalies
barriers	P-C-32: Dielectric Barriers for Arc Mitigation
Bayesian statistical model	P-A-27: A Method of Finding Optimal Parameters of Deep Charging Environmental Indicators by Using Orbital Anomaly Data of GEO Satellite
beam return	P-C-33: Enabling Electron Beam Use in Tenuous Space Plasmas using Plasma Contactors: the Ion Emission Model
bremsstrahlung x-rays	P-C-27: Method for Touchless Determination of Electrostatic Potential and Material Composition for Spacecraft
bulk charging	Long Term Charge Buildup and Dissipation in Spacecraft Materials
C
C-V characteristic	Study on Lorentz Force Characteristics of Electrodynamic Tether System Based on Hollow Cathode
Capacitance Matrix	P-C-8: Differential Charging Estimation of Spacecraft in Single and Double Maxwellian Plasma Environment
Carbon Nanotube Forests	P-C-21: Secondary Electron Yield Measurements of Carbon Nanotube Forests: Dependence on Morphology and Substrate
Carrier Mobility	P-C-23: Construction of Measurement System for Carrier Mobility in Insulating Materials for Spacecraft
change of relief of glass surfaces	P-A-15: Studying Interaction of Hot Magnetospheric Plasma with Spacecraft Solar Array Protective Coating
Charge accumulation	P-A-39: Analysis of Deterioration Phenomena on Fluorinated Insulating Material Irradiated by Proton and Electron
Charge and Discharge	P-C-23: Construction of Measurement System for Carrier Mobility in Insulating Materials for Spacecraft
Charge density	P-A-34*: Study of Internal Charging of Polymers through Numerical and Experimental Analyses - Comparison of Different Space used Numerical Tools
charge determination	P-C-27: Method for Touchless Determination of Electrostatic Potential and Material Composition for Spacecraft
charge dissipation	Long Term Charge Buildup and Dissipation in Spacecraft Materials
charge distribution	P-A-24: Measurement of Internal Charge Distribution in Dielectrics under High Energy Electron Irradiation
Charge transport	Physical and Spectrometric Analysis of Electron-Damaged LDPE P-A-34*: Study of Internal Charging of Polymers through Numerical and Experimental Analyses - Comparison of Different Space used Numerical Tools
charged dust transport	P-B-29*: Numerical Simulation of Charged Dust Transport around Irregularly Shaped Small Asteroids
Charging	P-C-9: Current Status of MUSCAT (Multi-Utility Spacecraft Charging analysis tools) P-A-21: Charging of geostationary satellite Electro-L2 in the Earth shadow The Suppression of Spacecraft Charging based on Nanographene Composite P-C-5: Improvement of the Spacecraft-Plasma Interaction Software (SPIS) with a New Versatile Architecture and Enhanced Modeling Capabilities for Electric Propulsion P-A-3: Updating the Europa Spacecraft Charging Environment Spacecraft Charging Material Properties Database P-C-19: Effect of Plume Interaction with Spacecraft Materials on Electron Emission Properties and Electrical Characteristics P-B-7: Surface Potential Measurement of Coverglass using Electron Beam and Ultraviolet as Charging Method Conductivity of Thermal Control White Paints as a Function of Temperature and Surface Voltage Overview of Activities Europe-wide and in France P-A-16*: XPS Investigation of the Source of GPS Arc Contamination Spacecraft Charging Study in Japan Electrical Ageing of Polymers under Space Radiation Environment
Charging analysis	P-C-30: Concerning of the Spacecraft Charging for Space Debris Removal and Orbital Services P-C-29: Detailed Charging Analysis of Exposed KAPTON in GSAT-19
Charging balance mode	Transient Characteristics of Charging Effects due to E-beam Irradiation: A Method of Charging Balance Mode
charging effect	The Defending Film of LEO Spacecraft High-voltage Solar Array Charging Effect Transient Characteristics of Charging Effects due to E-beam Irradiation: A Method of Charging Balance Mode
Charging Mitigation	Charging Behavior of the H-II Transfer Vehicle by Active Electron Emission Study on a Method of Stabilizing the Electron Emission of ELFs-charm
Charging of ionospheric sounding rockets with booms	P-C-11: Numerical Study on the Plasma Disturbance an Charging Processes by Booms of an Ionospheric Rocket
Charging simulations	Validation of Internal Charging Tools with REEF data
Chemical Vapor Deposition	P-C-21: Secondary Electron Yield Measurements of Carbon Nanotube Forests: Dependence on Morphology and Substrate
coating characteristics	P-C-31*: An Efficient Hybrid Approach for the Reduction of Secondary Electron Yield
composite materials	P-C-26: Electron Yield of Carbon-Composite Nanodielectric Material
Computational	P-B-36: Electron Range Computational Tool for Arbitrary Materials over a Wide Energy Range
Computer simulation	P-B-5: Plasma Plume Interaction with Chamber Walls during On ground Experiments: SPIS-EP Simulations and Comparison with Experiments Simulation of the Effect of Time-Dependent Electron Environment on the Internal Charging Dynamic using SPIS-IC
COMSOL	Preventing Electrostatic Discharge in the Mars 2020 PIXL X-Ray Tube
conductivity	P-C-18: Modification of Charge Body Migration in LDPE as a Result of Electron Radiation Exposure. P-A-34*: Study of Internal Charging of Polymers through Numerical and Experimental Analyses - Comparison of Different Space used Numerical Tools Conductivity of Thermal Control White Paints as a Function of Temperature and Surface Voltage
CONNEX	P-C-33: Enabling Electron Beam Use in Tenuous Space Plasmas using Plasma Contactors: the Ion Emission Model
Constant Voltage Conductivity	Time Evolved Constant Voltage Conductivity Measurements of Common Spaceborn Polymeric Materials
constellation	P-A-18: Nanosatellite Constellation for 3D Ionosphere Mapping
Contamination	The Case for GPS Arcing and High Satellite Arc Rates P-A-16*: XPS Investigation of the Source of GPS Arc Contamination
Contamination by charged dust	P-B-30: Ground Testing and Modelling of Dust Charging and Adhesion
Coulomb Actuation	P-A-4*: Low Earth Orbit Plasma Wake Shaping and Applications to On-Orbit Proximity Operations
Country Overview	Present Day Status of Spacecraft Charging Investigations in Russia
Coupled method	Advanced Numerical Schemes Implemented in SPIS to Improve the Accuracy of the Description of the Dense Cold and Drifting Plasma Populations
cover glasses of solar arrays	P-A-15: Studying Interaction of Hot Magnetospheric Plasma with Spacecraft Solar Array Protective Coating
Coverglass	P-B-7: Surface Potential Measurement of Coverglass using Electron Beam and Ultraviolet as Charging Method
Cryogenic temperature	P-C-13: Charging Characteristics of Electron Irradiated Polyimide Film under Cryogenic Temperature
cryogenic temperatures	P-B-4: Electrostatic Discharges from Conductive Thermal Coatings
cubesat	P-A-20: LEO Charging of the PICASSO Cubesat and Simulation of the Langmuir Probes Operation P-A-18: Nanosatellite Constellation for 3D Ionosphere Mapping
CubeSats	Impact of Miniaturized Fixed-bias Multi-Needle Langmuir Probes on CubeSats 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
Cuboid current collection	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
current waveform	P-A-30: Experimental and Numerical Characterizations of Current and Magnetic Fields Produced by Electrostatic Discharge due to Internal Charging
D
damage accumulation	P-A-31*: Effect of Damage Accumulation in Microcircuits under the Series of IESD
Dark Conductivity	Time Evolved Constant Voltage Conductivity Measurements of Common Spaceborn Polymeric Materials
database	Spacecraft Charging Material Properties Database
deep charging	Electric-Orbit-Raising Induced Deep Charging Requirement and Analysis of External Satellite Harness with Shields P-A-11: Prediction of the Outer Radiation Belt Variation by Kalman Filter based on Realtime Data of the Arase Satellite and Dst Index P-A-27: A Method of Finding Optimal Parameters of Deep Charging Environmental Indicators by Using Orbital Anomaly Data of GEO Satellite
deep dielectric charging	P-A-36: Experimental Study of Deep Dielectric Discharging of Polymer under Energetic Electron Irradiation
defending film	The Defending Film of LEO Spacecraft High-voltage Solar Array Charging Effect
degradation	P-A-39: Analysis of Deterioration Phenomena on Fluorinated Insulating Material Irradiated by Proton and Electron
Deorbit	Study on Lorentz Force Characteristics of Electrodynamic Tether System Based on Hollow Cathode
design criterion	P-B-18: Design and Experiment of Hollow-Cathode Plasma Contactor by a Kind of Criterion
df-PIC method	Advanced Numerical Schemes Implemented in SPIS to Improve the Accuracy of the Description of the Dense Cold and Drifting Plasma Populations
Dielectric charging	P-C-13: Charging Characteristics of Electron Irradiated Polyimide Film under Cryogenic Temperature P-A-26: Influence of Dielectric Charging on Microwave Discharge Process in Microwave Impedance Converter
dielectric ESD	P-A-30: Experimental and Numerical Characterizations of Current and Magnetic Fields Produced by Electrostatic Discharge due to Internal Charging
dielectric materials	Analysis of Charge Accumulation Phenomena by Physicochemical Analysis for Fluorinated Polymer Films Irradiated by Proton
Dielectrics	P-A-23: Internal Charging Issues Met during Electric Orbit Raising P-A-34*: Study of Internal Charging of Polymers through Numerical and Experimental Analyses - Comparison of Different Space used Numerical Tools Electrical Ageing of Polymers under Space Radiation Environment
different energy	P-A-24: Measurement of Internal Charge Distribution in Dielectrics under High Energy Electron Irradiation
different type and current	P-B-19: Instability of Potential Oscillations for Different Type and Current Hollow Cathode
discharge	Preventing Electrostatic Discharge in the Mars 2020 PIXL X-Ray Tube
Discharging	P-B-1: The Research of Small Space Debris Impact Inducing Discharge on High Voltage
Dispersive Transport	Time Evolved Constant Voltage Conductivity Measurements of Common Spaceborn Polymeric Materials
double Langmuir probe	P-A-17*: Mission Report of a Double Langmuir Probe Onboard HORYU-IV Satellite
dust and surface charging	*PLENARY TALK: The Effects of Dust Charging in Space and the Laboratory
dust charging	P-B-26: Electrostatic Dust Transportation due to Secondary Electron Emission and Surface Electric Field above the Lunar Terminator
Dust impact	The Effect of Plasma Cloud Expansion Associated with Dust Impacts
dust lofting	P-B-26: Electrostatic Dust Transportation due to Secondary Electron Emission and Surface Electric Field above the Lunar Terminator
dusty plasma	P-B-28*: Laboratory Investigations of Dusty Spacesuit Arcing in Plasma P-B-2: Laboratory Investigations of Electrostatic Discharge on Insulating Materials in Dusty Plasma
dusty space plasmas	*PLENARY TALK: The Effects of Dust Charging in Space and the Laboratory
E
E-beam irradiation	Transient Characteristics of Charging Effects due to E-beam Irradiation: A Method of Charging Balance Mode
ECEMP	P-A-30: Experimental and Numerical Characterizations of Current and Magnetic Fields Produced by Electrostatic Discharge due to Internal Charging
ECR	P-B-25: Plasma Particle Simulation of ECR Plasma Generation in Air Breathing Ion Engine (ABIE)
EDGE	P-A-35: Internal Charging Analysis of a Realistic Experiment with a Dedicated Modelling Chain
Electon irradiation	P-A-23: Internal Charging Issues Met during Electric Orbit Raising
Electric field	Electric-Orbit-Raising Induced Deep Charging Requirement and Analysis of External Satellite Harness with Shields P-A-34*: Study of Internal Charging of Polymers through Numerical and Experimental Analyses - Comparison of Different Space used Numerical Tools
Electric orbit raising	P-A-23: Internal Charging Issues Met during Electric Orbit Raising
electric propulsion	P-C-5: Improvement of the Spacecraft-Plasma Interaction Software (SPIS) with a New Versatile Architecture and Enhanced Modeling Capabilities for Electric Propulsion P-B-10: Model and Experimental Validation of Spacecraft-thruster Interactions for Electric Propulsion Thruster Plumes P-B-16: Testing and Simulation of the µCAT Plasma Plume P-B-21: Prototype Design of Surface Arc Thruster Coupling of a All-electric Spacecraft with its Plasma Plume and its Environment
Electric-Field Measurements	Simulation of the Electrostatic Environment of the Magnetospheric Multiscale Mission
electrical discharge	Correlations of Volatile Space Charging Environments with Aerospace Mechanism Friction Anomalies
electro cyclotron resonance	P-B-25: Plasma Particle Simulation of ECR Plasma Generation in Air Breathing Ion Engine (ABIE)
Electro-Acoustic	P-C-18: Modification of Charge Body Migration in LDPE as a Result of Electron Radiation Exposure.
electrodynamic tether	P-B-20: Electron Current Measurement of Electrodynamic Tether with Eliminating Current Collection at Tether Edge Charging Behavior of the H-II Transfer Vehicle by Active Electron Emission P-B-18: Design and Experiment of Hollow-Cathode Plasma Contactor by a Kind of Criterion Study on Lorentz Force Characteristics of Electrodynamic Tether System Based on Hollow Cathode
Electrodynamic Tether System	P-B-11: Effect of Periodic Attitude Libration on Long-term Orbital Dynamics of the Electrodynamic Tether System
electromagnetic environment	P-B-24: Particle Simulation on the Electromagnetic Environment of Ion Thruster Beam Neutralization
electron - hole	P-A-38: Characteristics of Electron - Hole Pairs Generation in Fluorinated Polymer Irradiated by an Electron
Electron Beam	P-C-23: Construction of Measurement System for Carrier Mobility in Insulating Materials for Spacecraft
electron beam bombardment	P-C-34: Dynamic Attenuation of Secondary Electrons Emission Yield of Fluorinated Polyimide Films
Electron Beams	P-C-33: Enabling Electron Beam Use in Tenuous Space Plasmas using Plasma Contactors: the Ion Emission Model P-A-1*: Orbital and Storm Analysis of the Pulsed Electrostatic Tractor using Statical Flux Distributions
electron deposition in materials	P-B-35: Transformation of Energy and Charge Deposition Profiles between Normally Incident and Isotropically Incident Electrons for Various Materials
Electron Emission	P-C-21: Secondary Electron Yield Measurements of Carbon Nanotube Forests: Dependence on Morphology and Substrate Worst-case Surface Charging: On the Importance of Measuring the Electron Emission Yield under Representative Environmental Conditions P-C-17*: On the Use of a Detailed Electron Emission Model for Spacecraft Charging at Low Energy
Electron emission yield	P-C-19: Effect of Plume Interaction with Spacecraft Materials on Electron Emission Properties and Electrical Characteristics
Electron emitter	Study on a Method of Stabilizing the Electron Emission of ELFs-charm
electron gun experiments	Radiation-induced Conductivity in Kapton-like Polymers Featuring Conductivity Rising with Accumulating Dose
electron irradiation	Physical and Spectrometric Analysis of Electron-Damaged LDPE
electron neutralization	P-B-24: Particle Simulation on the Electromagnetic Environment of Ion Thruster Beam Neutralization
Electron Range	P-B-36: Electron Range Computational Tool for Arbitrary Materials over a Wide Energy Range
electron spectra	P-C-37: Testing Materials under Electron Spectra Representative of GEO Worst-case Environments for Surface Charging
electron yield	P-C-25: Parameterization of Secondary and Backscattered Electron Yields for Spacecraft Charging P-C-24: Measurements of the Intrinsic Electron Yield of Highly Insulating Materials P-C-26: Electron Yield of Carbon-Composite Nanodielectric Material
electron-proton irradiation	P-A-15: Studying Interaction of Hot Magnetospheric Plasma with Spacecraft Solar Array Protective Coating
Electronics devices	Spacecraft Inner Charging Simulation of the Electronics Devices Plastic Cases
electrons	P-B-31: Techniques for Evaluating the Risk of Internal Space Charging on Long Time-Scale Orbits P-C-28*: Remote Sensing of Spacecraft Electrostatic Potential using Secondary Electrons
electrostatic	Preventing Electrostatic Discharge in the Mars 2020 PIXL X-Ray Tube
electrostatic discharge	P-B-4: Electrostatic Discharges from Conductive Thermal Coatings Electrostatic Testing of Multilayer Insulation for In-Space Cryogenic Vehicles P-B-6: Wireless Antenna Detection of Electrostatic Discharge Events P-B-2: Laboratory Investigations of Electrostatic Discharge on Insulating Materials in Dusty Plasma
Electrostatic discharges	P-A-15: Studying Interaction of Hot Magnetospheric Plasma with Spacecraft Solar Array Protective Coating P-A-34*: Study of Internal Charging of Polymers through Numerical and Experimental Analyses - Comparison of Different Space used Numerical Tools
Electrostatic discharges mitigation	P-A-28: Computer Simulations and Experimental Investigation for Heterodyne Characteristics on PCB with the Increased Resistance to Electrostatic Discharges
Electrostatic Risk	AMBER, The French Plasma Monitor onboard JASON3
Electrostatic Tractor	P-A-1*: Orbital and Storm Analysis of the Pulsed Electrostatic Tractor using Statical Flux Distributions
Electrothermal acceleration	P-B-21: Prototype Design of Surface Arc Thruster
ELFs-charm	Study on a Method of Stabilizing the Electron Emission of ELFs-charm
EMSES	P-B-25: Plasma Particle Simulation of ECR Plasma Generation in Air Breathing Ion Engine (ABIE)
energetic electron	P-A-36: Experimental Study of Deep Dielectric Discharging of Polymer under Energetic Electron Irradiation
energetic electrons	P-B-4: Electrostatic Discharges from Conductive Thermal Coatings
energy deposition profiles	P-B-35: Transformation of Energy and Charge Deposition Profiles between Normally Incident and Isotropically Incident Electrons for Various Materials
Energy distribution	P-C-17*: On the Use of a Detailed Electron Emission Model for Spacecraft Charging at Low Energy
EOR	Electric-Orbit-Raising Induced Deep Charging Requirement and Analysis of External Satellite Harness with Shields
EOS	P-A-31*: Effect of Damage Accumulation in Microcircuits under the Series of IESD
ERG	Suppression of Local Surface Charging on the ERG (Arase) Satellite
Erosion effect on electron emission	P-C-19: Effect of Plume Interaction with Spacecraft Materials on Electron Emission Properties and Electrical Characteristics
ESD	Preventing Electrostatic Discharge in the Mars 2020 PIXL X-Ray Tube P-C-32: Dielectric Barriers for Arc Mitigation Study on a Method of Stabilizing the Electron Emission of ELFs-charm Test Set-up Review for Arcing Test on New Solar Array Generation An Overview of Spacecraft Charging Research in India: Spacecraft Plasma Interaction Experiments—SPIX–III P-B-6: Wireless Antenna Detection of Electrostatic Discharge Events P-A-31*: Effect of Damage Accumulation in Microcircuits under the Series of IESD
evaluation	P-C-14: The Secondary Electron Emission Properties and the Influence on Charging Potentials
experiment and numerical calculations	Radiation-induced Conductivity in Kapton-like Polymers Featuring Conductivity Rising with Accumulating Dose
experimental internal charging	P-A-30: Experimental and Numerical Characterizations of Current and Magnetic Fields Produced by Electrostatic Discharge due to Internal Charging
Experimental testing	Validation of Internal Charging Tools with REEF data
extreme ultraviolet	P-C-16: Development of a Pulsed Supersonic Valve Aimed for Martian Atmospheric Simulation
F
Faraday Probe	P-B-16: Testing and Simulation of the µCAT Plasma Plume
FEA	Preventing Electrostatic Discharge in the Mars 2020 PIXL X-Ray Tube
FEM	Preventing Electrostatic Discharge in the Mars 2020 PIXL X-Ray Tube
Field Emission Cathode	Charging Behavior of the H-II Transfer Vehicle by Active Electron Emission
finding model parameters	Radiation-induced Conductivity in Kapton-like Polymers Featuring Conductivity Rising with Accumulating Dose
fitting experimental and theoretical results	Radiation-induced Conductivity in Kapton-like Polymers Featuring Conductivity Rising with Accumulating Dose
flexible solar array	Arcing Risk due to Micrometeorite/Debris Impact on Flexible Solar Array with 100V Bus Voltage
Fluorinated insulating materials	P-A-39: Analysis of Deterioration Phenomena on Fluorinated Insulating Material Irradiated by Proton and Electron
fluoroethylenepropylene	P-C-15: A Consideration of Degradation of Polymeric Materials in Sub-Low Earth Orbit Space Environment
forecast early warning	P-A-25: Study on Quantitative Evaluation Method for Charging Effect of Orbit Spacecraft
frame charging	P-A-2: Observations of Frame Charging by the MPS-LO Instrument on GOES-16
friction anomaly	Correlations of Volatile Space Charging Environments with Aerospace Mechanism Friction Anomalies
G
Galileo PLS	P-A-3: Updating the Europa Spacecraft Charging Environment
Geant4	P-A-32: Internal Charging Simulation for Satellite based on Reverse Monte Carlo Method
GEO	An Overview of Spacecraft Charging Research in India: Spacecraft Plasma Interaction Experiments—SPIX–III
GEO orbit	High-fidelity Multi-Length Scale Modeling of Spacecraft Charging in GEO Orbit
GEO Plasma	P-A-1*: Orbital and Storm Analysis of the Pulsed Electrostatic Tractor using Statical Flux Distributions
geomagnetic storm	Correlations of Volatile Space Charging Environments with Aerospace Mechanism Friction Anomalies
geostationary orbit	P-A-2: Observations of Frame Charging by the MPS-LO Instrument on GOES-16 Long Term Charge Buildup and Dissipation in Spacecraft Materials
geostationary spacecraft	P-A-21: Charging of geostationary satellite Electro-L2 in the Earth shadow
Global Positioning System	The Case for GPS Arcing and High Satellite Arc Rates
GOES-R	GOES-R-series Radiation Belt Observations in Support of Internal Charging Alerts and Investigations
GPS	P-A-14: Radiofrequency Interference from Satellite Solar Array Arcing
GPS and other MEO and GEO Arcing	USA Overview
graphene	The Suppression of Spacecraft Charging based on Nanographene Composite
GRAS	P-A-35: Internal Charging Analysis of a Realistic Experiment with a Dedicated Modelling Chain
Grid optics	P-B-17*: Effects of the Two-grid Optics on a Mini Gridded Helicon Ion Thruster
Gridded helicon ion thruster	P-B-17*: Effects of the Two-grid Optics on a Mini Gridded Helicon Ion Thruster
Gridded ion thruster	P-B-9*: Hybrid Fluid-Particle Plasma Modeling of a Radio-Frequency Gridded Ion Thruster
ground station network	P-A-18: Nanosatellite Constellation for 3D Ionosphere Mapping
Ground test	Electrostatic Testing of Multilayer Insulation for In-Space Cryogenic Vehicles
ground testing	P-B-14: Current Measurement of Backflow Ions from Ion Thruster for Estimation of Erosion Rate on HAYABUSA2 Surface Material P-B-12: Measurements of Backflow Ions from Ion Thruster for Evaluation of Surface Erosion on HAYABUSA2 P-B-28*: Laboratory Investigations of Dusty Spacesuit Arcing in Plasma P-B-2: Laboratory Investigations of Electrostatic Discharge on Insulating Materials in Dusty Plasma P-B-13: Energy Measurement of Backflow Ions from Ion Thruster for Estimation of Erosion Rate on HAYABUSA2 Surface Material
GSAT-19	P-C-29: Detailed Charging Analysis of Exposed KAPTON in GSAT-19
guidelines	P-A-33: Internal Electrostatic Discharge (iESD) Design Guidelines for Jovian Missions Guidelines for Space Weather Research and Operation discussed in Space Weather Expert Group (SWEG) in UNCOPUOS /LTS WG
H
Hall thrusters	Development of a Three-dimensional Electrostatic Code for Hall Thruster Plume and Spacecraft Interaction Analysis
Harness	Electric-Orbit-Raising Induced Deep Charging Requirement and Analysis of External Satellite Harness with Shields
HAYABUSA2 spacecraft	P-B-12: Measurements of Backflow Ions from Ion Thruster for Evaluation of Surface Erosion on HAYABUSA2
Helicon thruster	P-B-17*: Effects of the Two-grid Optics on a Mini Gridded Helicon Ion Thruster
Heterodyne characteristics on PCB with the increased resistance	P-A-28: Computer Simulations and Experimental Investigation for Heterodyne Characteristics on PCB with the Increased Resistance to Electrostatic Discharges
High energy electron	P-A-25: Study on Quantitative Evaluation Method for Charging Effect of Orbit Spacecraft
high energy electron enhance events	P-A-25: Study on Quantitative Evaluation Method for Charging Effect of Orbit Spacecraft
High voltage solar array	High Voltage Experiment Mission Results of HORYU-IV
high-fidelity simulation	High-fidelity Multi-Length Scale Modeling of Spacecraft Charging in GEO Orbit
high-voltage solar array	The Defending Film of LEO Spacecraft High-voltage Solar Array Charging Effect
Highly Disordered Insulating Materials	Time Evolved Constant Voltage Conductivity Measurements of Common Spaceborn Polymeric Materials
Hollow cathode	P-B-34: Plume Structure Study of Cathodic Plasma Contactor P-B-19: Instability of Potential Oscillations for Different Type and Current Hollow Cathode Study on Lorentz Force Characteristics of Electrodynamic Tether System Based on Hollow Cathode
hollow cathode keeper	P-B-8: 3D Printed Molybdenum for Grids and Keeper Electrodes in Ion Thruster
hollow-cathode plasma contactor	P-B-18: Design and Experiment of Hollow-Cathode Plasma Contactor by a Kind of Criterion
HTV	P-A-19: Result of Plasma Measurement in HTV during ISS Attached Phase Charging Behavior of the H-II Transfer Vehicle by Active Electron Emission
Hybrid fluid-particle simulation	P-B-9*: Hybrid Fluid-Particle Plasma Modeling of a Radio-Frequency Gridded Ion Thruster
Hybrid PIC code	P-B-32: Hybrid PIC Code for Active Shielding Demonstration Inspired from Magneto Plasma Sail
I
iESD	P-A-33: Internal Electrostatic Discharge (iESD) Design Guidelines for Jovian Missions Trapped Electron Environments of the Outer Planets
Impact	P-B-1: The Research of Small Space Debris Impact Inducing Discharge on High Voltage
in situ	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
in-situ measurement	Photoelectron Emission Current In-Situ Measurement of Space Material in Low Earth Orbit
instrument	P-A-35: Internal Charging Analysis of a Realistic Experiment with a Dedicated Modelling Chain
instrumentation	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
insulators	P-C-24: Measurements of the Intrinsic Electron Yield of Highly Insulating Materials P-C-26: Electron Yield of Carbon-Composite Nanodielectric Material
inter satellite ranging	P-A-18: Nanosatellite Constellation for 3D Ionosphere Mapping
interactions	P-B-10: Model and Experimental Validation of Spacecraft-thruster Interactions for Electric Propulsion Thruster Plumes
internal charging	P-A-28: Computer Simulations and Experimental Investigation for Heterodyne Characteristics on PCB with the Increased Resistance to Electrostatic Discharges P-B-31: Techniques for Evaluating the Risk of Internal Space Charging on Long Time-Scale Orbits P-A-23: Internal Charging Issues Met during Electric Orbit Raising P-A-35: Internal Charging Analysis of a Realistic Experiment with a Dedicated Modelling Chain P-A-32: Internal Charging Simulation for Satellite based on Reverse Monte Carlo Method Validation of Internal Charging Tools with REEF data GOES-R-series Radiation Belt Observations in Support of Internal Charging Alerts and Investigations P-C-35: Significance of Shielding Kernel Selection for Spacecraft Charging Assessments Simulation of the Effect of Time-Dependent Electron Environment on the Internal Charging Dynamic using SPIS-IC Status of Spacecraft Charging Study in China P-A-5: Tools for Understanding On-orbit Satellite Anomalies P-A-34*: Study of Internal Charging of Polymers through Numerical and Experimental Analyses - Comparison of Different Space used Numerical Tools Long Term Charge Buildup and Dissipation in Spacecraft Materials P-C-36: Improved Spacecraft Charging Roadmaps Developed to Support User Community Needs P-A-31*: Effect of Damage Accumulation in Microcircuits under the Series of IESD
internal charging effect	P-A-24: Measurement of Internal Charge Distribution in Dielectrics under High Energy Electron Irradiation
Ion beam	Improved Determination of Plasma Density Based on Spacecraft Potential of the Magnetospheric Multiscale Mission under Active Potential Control
ion emission	P-C-33: Enabling Electron Beam Use in Tenuous Space Plasmas using Plasma Contactors: the Ion Emission Model
ion optics	P-B-8: 3D Printed Molybdenum for Grids and Keeper Electrodes in Ion Thruster
ion thruster	P-B-14: Current Measurement of Backflow Ions from Ion Thruster for Estimation of Erosion Rate on HAYABUSA2 Surface Material P-B-17*: Effects of the Two-grid Optics on a Mini Gridded Helicon Ion Thruster P-B-15: Plume Potential Analysis for Ion Thruster Varying Spacecraft Potential by a Three-dimensional Electrostatic Full Particle Code P-B-8: 3D Printed Molybdenum for Grids and Keeper Electrodes in Ion Thruster P-B-13: Energy Measurement of Backflow Ions from Ion Thruster for Estimation of Erosion Rate on HAYABUSA2 Surface Material
ion thruster beam	P-B-24: Particle Simulation on the Electromagnetic Environment of Ion Thruster Beam Neutralization
Ion Thrusters	P-B-12: Measurements of Backflow Ions from Ion Thruster for Evaluation of Surface Erosion on HAYABUSA2
ionosphere	P-A-18: Nanosatellite Constellation for 3D Ionosphere Mapping
Ionospheric plasma	P-A-19: Result of Plasma Measurement in HTV during ISS Attached Phase P-A-13: Arcing on Solar Generators by Collection of Ionospheric Plasma Currents
Ionospheric plasma density measurement	Impact of Miniaturized Fixed-bias Multi-Needle Langmuir Probes on CubeSats
irradiation electron	P-A-38: Characteristics of Electron - Hole Pairs Generation in Fluorinated Polymer Irradiated by an Electron
ISO 11221	An Overview of Spacecraft Charging Research in India: Spacecraft Plasma Interaction Experiments—SPIX–III
ISS	P-A-19: Result of Plasma Measurement in HTV during ISS Attached Phase
J
Japan	Spacecraft Charging Study in Japan
Jason3	AMBER, The French Plasma Monitor onboard JASON3
Jovian environment	Modeling Surface Charging for NASA's Europa Clipper Mission
jovian missions	P-A-33: Internal Electrostatic Discharge (iESD) Design Guidelines for Jovian Missions
Jupiter	P-A-3: Updating the Europa Spacecraft Charging Environment
K
Kapton	P-C-22: Charging Analysis with Changing the Satellite Surface Material Property due to Space Environment
Kinetic Simulation	The Breakdown of the Fluid Approximation for Electrons in Mesothermal Plasma Expansion and Its Implications on Plasma Plume/Wake Models
Kinetic simulations	Impact of Miniaturized Fixed-bias Multi-Needle Langmuir Probes on CubeSats
L
Laboratory experiment	Test Set-up Review for Arcing Test on New Solar Array Generation
laboratory experiments	*PLENARY TALK: The Effects of Dust Charging in Space and the Laboratory
Langmuir	P-A-20: LEO Charging of the PICASSO Cubesat and Simulation of the Langmuir Probes Operation
Langmuir probe measurements	P-C-3: Simulations of Non-ideal Effects In Langmuir Probe Measurements
Langmuir Probes	P-C-4*: Simulations of the Rosetta Spacecraft Interaction with Comet Plasma
latent damage	P-A-31*: Effect of Damage Accumulation in Microcircuits under the Series of IESD
LDPE	Physical and Spectrometric Analysis of Electron-Damaged LDPE
LEO	P-A-6: Statistical Study of Surface-charging Events in Aurora Region over One Solar Cycle P-A-20: LEO Charging of the PICASSO Cubesat and Simulation of the Langmuir Probes Operation An Overview of Spacecraft Charging Research in India: Spacecraft Plasma Interaction Experiments—SPIX–III
LEO satellite anomalies	P-A-8: The Impact of Auroral Electron Streams on LEO Polar Satellites as a Source of Charging
local charging	Suppression of Local Surface Charging on the ERG (Arase) Satellite
Lorentz force characteristics	Study on Lorentz Force Characteristics of Electrodynamic Tether System Based on Hollow Cathode
low Earth orbit	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
Low incident electron energy	P-C-17*: On the Use of a Detailed Electron Emission Model for Spacecraft Charging at Low Energy
Low noise simulations	Advanced Numerical Schemes Implemented in SPIS to Improve the Accuracy of the Description of the Dense Cold and Drifting Plasma Populations
low-Earth orbit	P-C-12: Numerical Study on Plasma Disturbance near a Low-Earth Orbit Satellite
Lunar Dust	Numerical Modelling of the Lunar Exosphere and Lunar Lander Interactions with SPIS-DUST
Lunar dust simulants	P-B-30: Ground Testing and Modelling of Dust Charging and Adhesion
Lunar exosphere	Numerical Modelling of the Lunar Exosphere and Lunar Lander Interactions with SPIS-DUST
M
machine learning	P-A-5: Tools for Understanding On-orbit Satellite Anomalies
magnetic field	P-B-33: Comparison of Magnetospheric Magnetic Field Variations at Quasi-Zenith Orbit Based on Michibiki Observation and REPPU Global MHD Simulation
Magnetoplasma Sail	P-B-32: Hybrid PIC Code for Active Shielding Demonstration Inspired from Magneto Plasma Sail
magnetosphere plasma	P-A-21: Charging of geostationary satellite Electro-L2 in the Earth shadow
Magnetospheric Mission	Simulation of the Electrostatic Environment of the Magnetospheric Multiscale Mission
Mars2020	Preventing Electrostatic Discharge in the Mars 2020 PIXL X-Ray Tube
material	Spacecraft Charging Material Properties Database
material degradation	P-C-15: A Consideration of Degradation of Polymeric Materials in Sub-Low Earth Orbit Space Environment
material determination	P-C-27: Method for Touchless Determination of Electrostatic Potential and Material Composition for Spacecraft
Material Properties	P-B-36: Electron Range Computational Tool for Arbitrary Materials over a Wide Energy Range
materials	P-C-26: Electron Yield of Carbon-Composite Nanodielectric Material
Materials Aging	USA Overview
Materials Testing	P-B-3: Materials Charging Investigations for Solar Orbiter
measurement	P-A-21: Charging of geostationary satellite Electro-L2 in the Earth shadow P-C-14: The Secondary Electron Emission Properties and the Influence on Charging Potentials
measurement of backflow current	P-B-14: Current Measurement of Backflow Ions from Ion Thruster for Estimation of Erosion Rate on HAYABUSA2 Surface Material
measurement of backflow energy	P-B-13: Energy Measurement of Backflow Ions from Ion Thruster for Estimation of Erosion Rate on HAYABUSA2 Surface Material
mechanism anomalies	Correlations of Volatile Space Charging Environments with Aerospace Mechanism Friction Anomalies
Medium Earth Orbit (MEO)	P-A-9: Statistical Analysis of Spacecraft Charging Environment in the Medium Earth Orbit
Meso-thermal magnetized plasma	P-C-3: Simulations of Non-ideal Effects In Langmuir Probe Measurements
Method of Moments	P-C-8: Differential Charging Estimation of Spacecraft in Single and Double Maxwellian Plasma Environment
MHD simulation	P-B-33: Comparison of Magnetospheric Magnetic Field Variations at Quasi-Zenith Orbit Based on Michibiki Observation and REPPU Global MHD Simulation
MICHIBIKI Satellite	P-A-10*: Surface Charging Analysis of the Quasi-Zenith Satellite “MICHIBIKI”
Micro-Cathode Arc Thruster	P-B-16: Testing and Simulation of the µCAT Plasma Plume
micro-structured surface	P-C-31*: An Efficient Hybrid Approach for the Reduction of Secondary Electron Yield
microcircuits	P-A-31*: Effect of Damage Accumulation in Microcircuits under the Series of IESD
micrometeorites and debris	Arcing Risk due to Micrometeorite/Debris Impact on Flexible Solar Array with 100V Bus Voltage
Microwave Discharge	P-A-26: Influence of Dielectric Charging on Microwave Discharge Process in Microwave Impedance Converter
Microwave Impedance Converter	P-A-26: Influence of Dielectric Charging on Microwave Discharge Process in Microwave Impedance Converter
model	P-B-10: Model and Experimental Validation of Spacecraft-thruster Interactions for Electric Propulsion Thruster Plumes
modeling	P-A-21: Charging of geostationary satellite Electro-L2 in the Earth shadow P-C-35: Significance of Shielding Kernel Selection for Spacecraft Charging Assessments P-C-25: Parameterization of Secondary and Backscattered Electron Yields for Spacecraft Charging 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 Coupling of a All-electric Spacecraft with its Plasma Plume and its Environment
modelling chain	P-A-35: Internal Charging Analysis of a Realistic Experiment with a Dedicated Modelling Chain
molybdenum	P-B-8: 3D Printed Molybdenum for Grids and Keeper Electrodes in Ion Thruster
Moon	Numerical Modelling of the Lunar Exosphere and Lunar Lander Interactions with SPIS-DUST
MoORa	P-A-35: Internal Charging Analysis of a Realistic Experiment with a Dedicated Modelling Chain
multi-needle Langmuir probe	P-A-22: Multi-needle Langmuir Probe Operation and Acute Probe Current Susceptibility to Spacecraft Potential
Multi-Needle Langmuir Probes	Impact of Miniaturized Fixed-bias Multi-Needle Langmuir Probes on CubeSats
multi-physic	P-A-35: Internal Charging Analysis of a Realistic Experiment with a Dedicated Modelling Chain
Multilayer Insulation	Electrostatic Testing of Multilayer Insulation for In-Space Cryogenic Vehicles
MUSCAT	P-C-9: Current Status of MUSCAT (Multi-Utility Spacecraft Charging analysis tools)
N
nano satellite	Photoelectron Emission Current In-Situ Measurement of Space Material in Low Earth Orbit P-A-18: Nanosatellite Constellation for 3D Ionosphere Mapping
Nanosatellite	P-B-23: Development of Vacuum Arc Thruster with Plasma Interaction Ignition for Nanosatellite High Voltage Experiment Mission Results of HORYU-IV
NASCAP	P-C-29: Detailed Charging Analysis of Exposed KAPTON in GSAT-19
NASCAP2K	Modeling Surface Charging for NASA's Europa Clipper Mission
Near-Earth Space Environment	Quantifying Spacecraft Specific Surface-Charging Risk in Geostationary Orbit
neutral gas	P-B-20: Electron Current Measurement of Electrodynamic Tether with Eliminating Current Collection at Tether Edge
neutralization	P-C-33: Enabling Electron Beam Use in Tenuous Space Plasmas using Plasma Contactors: the Ion Emission Model
New Solar Array Designs	USA Overview
New Spacecraft Materials	USA Overview
nitrogen	P-C-15: A Consideration of Degradation of Polymeric Materials in Sub-Low Earth Orbit Space Environment
Numerical simulation	P-C-2: Spacecraft Surface Charging Simulation based on 3D Electrostatic PIC Model Development of a Three-dimensional Electrostatic Code for Hall Thruster Plume and Spacecraft Interaction Analysis Numerical Modelling of the Lunar Exosphere and Lunar Lander Interactions with SPIS-DUST P-B-15: Plume Potential Analysis for Ion Thruster Varying Spacecraft Potential by a Three-dimensional Electrostatic Full Particle Code
NUMIT	P-B-35: Transformation of Energy and Charge Deposition Profiles between Normally Incident and Isotropically Incident Electrons for Various Materials
O
On orbit measurements	AMBER, The French Plasma Monitor onboard JASON3
On-ground experiments	P-B-5: Plasma Plume Interaction with Chamber Walls during On ground Experiments: SPIS-EP Simulations and Comparison with Experiments
On-orbit investigations	P-C-36: Improved Spacecraft Charging Roadmaps Developed to Support User Community Needs
Orbital Dynamics	P-B-11: Effect of Periodic Attitude Libration on Long-term Orbital Dynamics of the Electrodynamic Tether System
Orbital Elements	P-B-11: Effect of Periodic Attitude Libration on Long-term Orbital Dynamics of the Electrodynamic Tether System
OSR	Analysis of Charge Accumulation Phenomena by Physicochemical Analysis for Fluorinated Polymer Films Irradiated by Proton
Outer Planets	Trapped Electron Environments of the Outer Planets
Overview	Status of Spacecraft Charging Study in China Overview of Activities Europe-wide and in France
P
paint	P-B-4: Electrostatic Discharges from Conductive Thermal Coatings
Particle in Cell	P-A-8: The Impact of Auroral Electron Streams on LEO Polar Satellites as a Source of Charging
Particle-in-cell simulation	P-B-24: Particle Simulation on the Electromagnetic Environment of Ion Thruster Beam Neutralization P-C-12: Numerical Study on Plasma Disturbance near a Low-Earth Orbit Satellite
Particle-in-cell simulations	P-C-7: Wake Formation behind Small Satellites
PEA	P-A-24: Measurement of Internal Charge Distribution in Dielectrics under High Energy Electron Irradiation P-C-18: Modification of Charge Body Migration in LDPE as a Result of Electron Radiation Exposure.
penetrating radiation	P-A-27: A Method of Finding Optimal Parameters of Deep Charging Environmental Indicators by Using Orbital Anomaly Data of GEO Satellite
Photo Voltaic Assembly	Test Set-up Review for Arcing Test on New Solar Array Generation
photoelectron	P-C-22: Charging Analysis with Changing the Satellite Surface Material Property due to Space Environment P-C-10: Particle Simulation Analysis of Spacecraft Charging Processes in Plasma Wave Environment Numerical Simulation of Spacecraft Charging Processes in Time-varying Plasma Environment
photoelectron current	Photoelectron Emission Current In-Situ Measurement of Space Material in Low Earth Orbit
photoemission	P-A-22: Multi-needle Langmuir Probe Operation and Acute Probe Current Susceptibility to Spacecraft Potential
PiC	Numerical Modelling of the Lunar Exosphere and Lunar Lander Interactions with SPIS-DUST
PIC Method	P-B-16: Testing and Simulation of the µCAT Plasma Plume
PIC simulation	P-C-10: Particle Simulation Analysis of Spacecraft Charging Processes in Plasma Wave Environment Numerical Simulation of Spacecraft Charging Processes in Time-varying Plasma Environment
PIC simulations	P-C-3: Simulations of Non-ideal Effects In Langmuir Probe Measurements
PIXL	Preventing Electrostatic Discharge in the Mars 2020 PIXL X-Ray Tube
plasma	P-B-23: Development of Vacuum Arc Thruster with Plasma Interaction Ignition for Nanosatellite P-A-17*: Mission Report of a Double Langmuir Probe Onboard HORYU-IV Satellite P-B-10: Model and Experimental Validation of Spacecraft-thruster Interactions for Electric Propulsion Thruster Plumes P-B-20: Electron Current Measurement of Electrodynamic Tether with Eliminating Current Collection at Tether Edge P-A-15: Studying Interaction of Hot Magnetospheric Plasma with Spacecraft Solar Array Protective Coating P-A-3: Updating the Europa Spacecraft Charging Environment P-C-4*: Simulations of the Rosetta Spacecraft Interaction with Comet Plasma Numerical Modelling of the Lunar Exosphere and Lunar Lander Interactions with SPIS-DUST 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 P-C-1: Simulation and Analysis of the SMILE Charging using SPIS High-fidelity Multi-Length Scale Modeling of Spacecraft Charging in GEO Orbit P-C-30: Concerning of the Spacecraft Charging for Space Debris Removal and Orbital Services P-C-29: Detailed Charging Analysis of Exposed KAPTON in GSAT-19
Plasma Arcing	P-A-14: Radiofrequency Interference from Satellite Solar Array Arcing
Plasma Cloud	The Effect of Plasma Cloud Expansion Associated with Dust Impacts
Plasma contactor	P-B-34: Plume Structure Study of Cathodic Plasma Contactor P-C-33: Enabling Electron Beam Use in Tenuous Space Plasmas using Plasma Contactors: the Ion Emission Model
Plasma density	Improved Determination of Plasma Density Based on Spacecraft Potential of the Magnetospheric Multiscale Mission under Active Potential Control
Plasma Detector	AMBER, The French Plasma Monitor onboard JASON3
Plasma diagnostics	P-B-17*: Effects of the Two-grid Optics on a Mini Gridded Helicon Ion Thruster
Plasma disturbances	P-C-11: Numerical Study on the Plasma Disturbance an Charging Processes by Booms of an Ionospheric Rocket
plasma environment	P-A-2: Observations of Frame Charging by the MPS-LO Instrument on GOES-16 P-A-9: Statistical Analysis of Spacecraft Charging Environment in the Medium Earth Orbit Spacecraft Potential Estimation in Worst Case Environment
Plasma Expansion	The Breakdown of the Fluid Approximation for Electrons in Mesothermal Plasma Expansion and Its Implications on Plasma Plume/Wake Models
plasma generation	P-B-25: Plasma Particle Simulation of ECR Plasma Generation in Air Breathing Ion Engine (ABIE)
plasma injection	P-B-33: Comparison of Magnetospheric Magnetic Field Variations at Quasi-Zenith Orbit Based on Michibiki Observation and REPPU Global MHD Simulation
plasma interaction	Evidence for Arcing on the International Space Station Solar Arrays
Plasma measurement	P-A-19: Result of Plasma Measurement in HTV during ISS Attached Phase
plasma particle simulation	P-B-25: Plasma Particle Simulation of ECR Plasma Generation in Air Breathing Ion Engine (ABIE)
Plasma Physics	P-B-32: Hybrid PIC Code for Active Shielding Demonstration Inspired from Magneto Plasma Sail
plasma plume	Coupling of a All-electric Spacecraft with its Plasma Plume and its Environment
Plasma propulsion	The Breakdown of the Fluid Approximation for Electrons in Mesothermal Plasma Expansion and Its Implications on Plasma Plume/Wake Models P-B-5: Plasma Plume Interaction with Chamber Walls during On ground Experiments: SPIS-EP Simulations and Comparison with Experiments P-B-9*: Hybrid Fluid-Particle Plasma Modeling of a Radio-Frequency Gridded Ion Thruster
Plasma simulation	P-B-9*: Hybrid Fluid-Particle Plasma Modeling of a Radio-Frequency Gridded Ion Thruster
Plasma surface interaction	P-B-5: Plasma Plume Interaction with Chamber Walls during On ground Experiments: SPIS-EP Simulations and Comparison with Experiments
Plasma Wake	P-A-4*: Low Earth Orbit Plasma Wake Shaping and Applications to On-Orbit Proximity Operations
Plasma wakes	P-C-11: Numerical Study on the Plasma Disturbance an Charging Processes by Booms of an Ionospheric Rocket
plasma wave	P-C-10: Particle Simulation Analysis of Spacecraft Charging Processes in Plasma Wave Environment Numerical Simulation of Spacecraft Charging Processes in Time-varying Plasma Environment
Plastic cases	Spacecraft Inner Charging Simulation of the Electronics Devices Plastic Cases
plume	P-B-10: Model and Experimental Validation of Spacecraft-thruster Interactions for Electric Propulsion Thruster Plumes
Plume effect	P-C-19: Effect of Plume Interaction with Spacecraft Materials on Electron Emission Properties and Electrical Characteristics
Plume structure	P-B-34: Plume Structure Study of Cathodic Plasma Contactor
polar	P-A-20: LEO Charging of the PICASSO Cubesat and Simulation of the Langmuir Probes Operation
polyimide	P-C-13: Charging Characteristics of Electron Irradiated Polyimide Film under Cryogenic Temperature P-C-15: A Consideration of Degradation of Polymeric Materials in Sub-Low Earth Orbit Space Environment
polyimide film	P-C-34: Dynamic Attenuation of Secondary Electrons Emission Yield of Fluorinated Polyimide Films
Polymers	P-A-34*: Study of Internal Charging of Polymers through Numerical and Experimental Analyses - Comparison of Different Space used Numerical Tools Electrical Ageing of Polymers under Space Radiation Environment
potential	P-C-28*: Remote Sensing of Spacecraft Electrostatic Potential using Secondary Electrons
potential oscillations	P-B-19: Instability of Potential Oscillations for Different Type and Current Hollow Cathode
probe	P-A-20: LEO Charging of the PICASSO Cubesat and Simulation of the Langmuir Probes Operation
Proton beam	P-A-39: Analysis of Deterioration Phenomena on Fluorinated Insulating Material Irradiated by Proton and Electron
proton irradiation	Analysis of Charge Accumulation Phenomena by Physicochemical Analysis for Fluorinated Polymer Films Irradiated by Proton
PTFE	P-A-36: Experimental Study of Deep Dielectric Discharging of Polymer under Energetic Electron Irradiation
Pulsed	P-C-18: Modification of Charge Body Migration in LDPE as a Result of Electron Radiation Exposure.
pulsed electroacoustic method	P-A-38: Characteristics of Electron - Hole Pairs Generation in Fluorinated Polymer Irradiated by an Electron
pulsed supersonic valve	P-C-16: Development of a Pulsed Supersonic Valve Aimed for Martian Atmospheric Simulation
Q
Qualification Test	Test Set-up Review for Arcing Test on New Solar Array Generation
Quasi-Zenith Satellite	P-A-10*: Surface Charging Analysis of the Quasi-Zenith Satellite “MICHIBIKI”
R
Radiation	P-A-35: Internal Charging Analysis of a Realistic Experiment with a Dedicated Modelling Chain P-C-18: Modification of Charge Body Migration in LDPE as a Result of Electron Radiation Exposure. P-A-39: Analysis of Deterioration Phenomena on Fluorinated Insulating Material Irradiated by Proton and Electron
Radiation Belt Forecasts	P-A-11: Prediction of the Outer Radiation Belt Variation by Kalman Filter based on Realtime Data of the Arase Satellite and Dst Index
radiation belts	GOES-R-series Radiation Belt Observations in Support of Internal Charging Alerts and Investigations Long Term Charge Buildup and Dissipation in Spacecraft Materials
Radiation dose	Electrical Ageing of Polymers under Space Radiation Environment
Radiation Shielding	P-B-32: Hybrid PIC Code for Active Shielding Demonstration Inspired from Magneto Plasma Sail
Radiations	P-A-34*: Study of Internal Charging of Polymers through Numerical and Experimental Analyses - Comparison of Different Space used Numerical Tools
Radio frequency plasma	P-B-17*: Effects of the Two-grid Optics on a Mini Gridded Helicon Ion Thruster
remote	P-C-28*: Remote Sensing of Spacecraft Electrostatic Potential using Secondary Electrons
resistivitiy	P-C-18: Modification of Charge Body Migration in LDPE as a Result of Electron Radiation Exposure.
resistivity	Electric-Orbit-Raising Induced Deep Charging Requirement and Analysis of External Satellite Harness with Shields
Reverse Monte Carlo	P-A-32: Internal Charging Simulation for Satellite based on Reverse Monte Carlo Method
RF sheath	Numerical Simulation of Spacecraft Charging Processes in Time-varying Plasma Environment
RFI	P-A-14: Radiofrequency Interference from Satellite Solar Array Arcing
Russia	Present Day Status of Spacecraft Charging Investigations in Russia
S
satellite	Suppression of Local Surface Charging on the ERG (Arase) Satellite P-A-34*: Study of Internal Charging of Polymers through Numerical and Experimental Analyses - Comparison of Different Space used Numerical Tools
satellite anomalies	P-A-5: Tools for Understanding On-orbit Satellite Anomalies
Satellite Arcing Rates	The Case for GPS Arcing and High Satellite Arc Rates
Satellite charging	P-A-8: The Impact of Auroral Electron Streams on LEO Polar Satellites as a Source of Charging
Satellite design	P-C-30: Concerning of the Spacecraft Charging for Space Debris Removal and Orbital Services
secondary	P-C-28*: Remote Sensing of Spacecraft Electrostatic Potential using Secondary Electrons
secondary electron	The Suppression of Spacecraft Charging based on Nanographene Composite
secondary electron emission	P-B-26: Electrostatic Dust Transportation due to Secondary Electron Emission and Surface Electric Field above the Lunar Terminator P-C-14: The Secondary Electron Emission Properties and the Influence on Charging Potentials
Secondary Electron Yield	P-C-8: Differential Charging Estimation of Spacecraft in Single and Double Maxwellian Plasma Environment P-C-21: Secondary Electron Yield Measurements of Carbon Nanotube Forests: Dependence on Morphology and Substrate P-C-31*: An Efficient Hybrid Approach for the Reduction of Secondary Electron Yield
secondary electrons emission yield	P-C-34: Dynamic Attenuation of Secondary Electrons Emission Yield of Fluorinated Polyimide Films
selective laser melting	P-B-8: 3D Printed Molybdenum for Grids and Keeper Electrodes in Ion Thruster
sensing	P-C-28*: Remote Sensing of Spacecraft Electrostatic Potential using Secondary Electrons
silica dust	P-B-26: Electrostatic Dust Transportation due to Secondary Electron Emission and Surface Electric Field above the Lunar Terminator
simulation	Preventing Electrostatic Discharge in the Mars 2020 PIXL X-Ray Tube P-C-5: Improvement of the Spacecraft-Plasma Interaction Software (SPIS) with a New Versatile Architecture and Enhanced Modeling Capabilities for Electric Propulsion Coupling of a All-electric Spacecraft with its Plasma Plume and its Environment
Simulations	Quantifying Spacecraft Specific Surface-Charging Risk in Geostationary Orbit
small satellite	P-A-17*: Mission Report of a Double Langmuir Probe Onboard HORYU-IV Satellite
SMILE	P-C-1: Simulation and Analysis of the SMILE Charging using SPIS
software	P-A-35: Internal Charging Analysis of a Realistic Experiment with a Dedicated Modelling Chain
solar array	Modeling Surface Charging for NASA's Europa Clipper Mission Test Set-up Review for Arcing Test on New Solar Array Generation P-A-13: Arcing on Solar Generators by Collection of Ionospheric Plasma Currents Evidence for Arcing on the International Space Station Solar Arrays
Solar array arcing	High Voltage Experiment Mission Results of HORYU-IV
Solar Array Plasma Interactions	P-A-16*: XPS Investigation of the Source of GPS Arc Contamination
Solar Cycle	P-A-6: Statistical Study of Surface-charging Events in Aurora Region over One Solar Cycle
Solar Orbiter	P-B-3: Materials Charging Investigations for Solar Orbiter
Solar Panel	Test Set-up Review for Arcing Test on New Solar Array Generation
Solar panels	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
space anomalies	P-A-27: A Method of Finding Optimal Parameters of Deep Charging Environmental Indicators by Using Orbital Anomaly Data of GEO Satellite
space charge	Analysis of Charge Accumulation Phenomena by Physicochemical Analysis for Fluorinated Polymer Films Irradiated by Proton
Space charge accumulation	P-A-38: Characteristics of Electron - Hole Pairs Generation in Fluorinated Polymer Irradiated by an Electron
Space Debris	P-A-1*: Orbital and Storm Analysis of the Pulsed Electrostatic Tractor using Statical Flux Distributions P-B-1: The Research of Small Space Debris Impact Inducing Discharge on High Voltage
space environment	P-A-17*: Mission Report of a Double Langmuir Probe Onboard HORYU-IV Satellite P-C-23: Construction of Measurement System for Carrier Mobility in Insulating Materials for Spacecraft Simulation of the Effect of Time-Dependent Electron Environment on the Internal Charging Dynamic using SPIS-IC
Space plasma physics	P-C-3: Simulations of Non-ideal Effects In Langmuir Probe Measurements
space plasmas	P-C-33: Enabling Electron Beam Use in Tenuous Space Plasmas using Plasma Contactors: the Ion Emission Model
space solar array	Arcing Risk due to Micrometeorite/Debris Impact on Flexible Solar Array with 100V Bus Voltage
Space Weather	P-C-35: Significance of Shielding Kernel Selection for Spacecraft Charging Assessments Guidelines for Space Weather Research and Operation discussed in Space Weather Expert Group (SWEG) in UNCOPUOS /LTS WG P-A-7*: Development of a Real-time Risk Estimation Method of Spacecraft Surface Charging Quantifying Spacecraft Specific Surface-Charging Risk in Geostationary Orbit P-A-16*: XPS Investigation of the Source of GPS Arc Contamination P-C-36: Improved Spacecraft Charging Roadmaps Developed to Support User Community Needs
Spacecraft	P-C-23: Construction of Measurement System for Carrier Mobility in Insulating Materials for Spacecraft P-C-28*: Remote Sensing of Spacecraft Electrostatic Potential using Secondary Electrons Spacecraft Charging Study in Japan
Spacecraft Arcing	Arc Plasma Propagation and Arc Current Profiles
spacecraft charge	P-A-25: Study on Quantitative Evaluation Method for Charging Effect of Orbit Spacecraft
spacecraft charging	P-C-32: Dielectric Barriers for Arc Mitigation AMBER, The French Plasma Monitor onboard JASON3 P-B-31: Techniques for Evaluating the Risk of Internal Space Charging on Long Time-Scale Orbits P-C-23: Construction of Measurement System for Carrier Mobility in Insulating Materials for Spacecraft P-C-4*: Simulations of the Rosetta Spacecraft Interaction with Comet Plasma P-C-10: Particle Simulation Analysis of Spacecraft Charging Processes in Plasma Wave Environment P-C-25: Parameterization of Secondary and Backscattered Electron Yields for Spacecraft Charging 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 Study on a Method of Stabilizing the Electron Emission of ELFs-charm 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 The Case for GPS Arcing and High Satellite Arc Rates Numerical Simulation of Spacecraft Charging Processes in Time-varying Plasma Environment P-C-17*: On the Use of a Detailed Electron Emission Model for Spacecraft Charging at Low Energy Test Set-up Review for Arcing Test on New Solar Array Generation P-B-35: Transformation of Energy and Charge Deposition Profiles between Normally Incident and Isotropically Incident Electrons for Various Materials High-fidelity Multi-Length Scale Modeling of Spacecraft Charging in GEO Orbit Quantifying Spacecraft Specific Surface-Charging Risk in Geostationary Orbit P-C-12: Numerical Study on Plasma Disturbance near a Low-Earth Orbit Satellite P-C-7: Wake Formation behind Small Satellites P-C-24: Measurements of the Intrinsic Electron Yield of Highly Insulating Materials P-C-31*: An Efficient Hybrid Approach for the Reduction of Secondary Electron Yield P-C-26: Electron Yield of Carbon-Composite Nanodielectric Material Spacecraft Potential Estimation in Worst Case Environment P-A-31*: Effect of Damage Accumulation in Microcircuits under the Series of IESD
Spacecraft charging assessment	Worst-case Surface Charging: On the Importance of Measuring the Electron Emission Yield under Representative Environmental Conditions
Spacecraft Charging fro LEO and Mars Missions	USA Overview
Spacecraft Charging Investigations	Present Day Status of Spacecraft Charging Investigations in Russia
Spacecraft discharging alert	P-A-7*: Development of a Real-time Risk Estimation Method of Spacecraft Surface Charging
spacecraft environment modeling	P-B-35: Transformation of Energy and Charge Deposition Profiles between Normally Incident and Isotropically Incident Electrons for Various Materials
Spacecraft inner charging	Spacecraft Inner Charging Simulation of the Electronics Devices Plastic Cases
Spacecraft Plasma Interaction Modelling	Simulation of the Electrostatic Environment of the Magnetospheric Multiscale Mission
Spacecraft potential	The Effect of Plasma Cloud Expansion Associated with Dust Impacts P-A-22: Multi-needle Langmuir Probe Operation and Acute Probe Current Susceptibility to Spacecraft Potential
Spacecraft potential control	Improved Determination of Plasma Density Based on Spacecraft Potential of the Magnetospheric Multiscale Mission under Active Potential Control Simulation of the Electrostatic Environment of the Magnetospheric Multiscale Mission
Spacecraft Power Systems	The Case for GPS Arcing and High Satellite Arc Rates
spacecraft surface charging	P-C-37: Testing Materials under Electron Spectra Representative of GEO Worst-case Environments for Surface Charging P-A-9: Statistical Analysis of Spacecraft Charging Environment in the Medium Earth Orbit P-A-7*: Development of a Real-time Risk Estimation Method of Spacecraft Surface Charging
Spacecraft-Plasma Interaction	P-C-4*: Simulations of the Rosetta Spacecraft Interaction with Comet Plasma P-A-4*: Low Earth Orbit Plasma Wake Shaping and Applications to On-Orbit Proximity Operations P-C-7: Wake Formation behind Small Satellites
spacesuit charging	P-B-28*: Laboratory Investigations of Dusty Spacesuit Arcing in Plasma
SPIS	P-C-5: Improvement of the Spacecraft-Plasma Interaction Software (SPIS) with a New Versatile Architecture and Enhanced Modeling Capabilities for Electric Propulsion P-C-4*: Simulations of the Rosetta Spacecraft Interaction with Comet Plasma 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 P-C-1: Simulation and Analysis of the SMILE Charging using SPIS Advanced Numerical Schemes Implemented in SPIS to Improve the Accuracy of the Description of the Dense Cold and Drifting Plasma Populations Coupling of a All-electric Spacecraft with its Plasma Plume and its Environment
SPIS simulation	P-B-30: Ground Testing and Modelling of Dust Charging and Adhesion
SPIS-IC	P-A-35: Internal Charging Analysis of a Realistic Experiment with a Dedicated Modelling Chain
SPIX	An Overview of Spacecraft Charging Research in India: Spacecraft Plasma Interaction Experiments—SPIX–III
Standards	P-C-36: Improved Spacecraft Charging Roadmaps Developed to Support User Community Needs
Storage conditions	Worst-case Surface Charging: On the Importance of Measuring the Electron Emission Yield under Representative Environmental Conditions
Sub-LEO	P-C-15: A Consideration of Degradation of Polymeric Materials in Sub-Low Earth Orbit Space Environment
suppression	The Suppression of Spacecraft Charging based on Nanographene Composite
Surface arc discharge	P-B-21: Prototype Design of Surface Arc Thruster
surface charging	Modeling Surface Charging for NASA's Europa Clipper Mission P-A-6: Statistical Study of Surface-charging Events in Aurora Region over One Solar Cycle P-B-33: Comparison of Magnetospheric Magnetic Field Variations at Quasi-Zenith Orbit Based on Michibiki Observation and REPPU Global MHD Simulation Status of Spacecraft Charging Study in China P-C-1: Simulation and Analysis of the SMILE Charging using SPIS P-A-10*: Surface Charging Analysis of the Quasi-Zenith Satellite “MICHIBIKI” P-C-14: The Secondary Electron Emission Properties and the Influence on Charging Potentials P-C-36: Improved Spacecraft Charging Roadmaps Developed to Support User Community Needs
surface charging effect	P-C-2: Spacecraft Surface Charging Simulation based on 3D Electrostatic PIC Model
Surface erosion	P-B-12: Measurements of Backflow Ions from Ion Thruster for Evaluation of Surface Erosion on HAYABUSA2
surface erosion of spacecraft	P-B-14: Current Measurement of Backflow Ions from Ion Thruster for Estimation of Erosion Rate on HAYABUSA2 Surface Material P-B-13: Energy Measurement of Backflow Ions from Ion Thruster for Estimation of Erosion Rate on HAYABUSA2 Surface Material
Surface Potential	P-B-7: Surface Potential Measurement of Coverglass using Electron Beam and Ultraviolet as Charging Method
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TARANIS	Advanced Numerical Schemes Implemented in SPIS to Improve the Accuracy of the Description of the Dense Cold and Drifting Plasma Populations
Temperature Dependence	P-B-3: Materials Charging Investigations for Solar Orbiter
tenuous plasmas	P-C-33: Enabling Electron Beam Use in Tenuous Space Plasmas using Plasma Contactors: the Ion Emission Model
test	P-A-31*: Effect of Damage Accumulation in Microcircuits under the Series of IESD
Tethers	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
Theory	P-B-36: Electron Range Computational Tool for Arbitrary Materials over a Wide Energy Range
Thermal control	P-B-4: Electrostatic Discharges from Conductive Thermal Coatings
threshold of failure	P-A-31*: Effect of Damage Accumulation in Microcircuits under the Series of IESD
Thruster	P-B-23: Development of Vacuum Arc Thruster with Plasma Interaction Ignition for Nanosatellite
Thruster plume and spacecraft interactions	Development of a Three-dimensional Electrostatic Code for Hall Thruster Plume and Spacecraft Interaction Analysis
thruster plume potential	P-B-15: Plume Potential Analysis for Ion Thruster Varying Spacecraft Potential by a Three-dimensional Electrostatic Full Particle Code
Top-Hat	AMBER, The French Plasma Monitor onboard JASON3
Total Electron Emission Yield	P-C-22: Charging Analysis with Changing the Satellite Surface Material Property due to Space Environment
Transient characteristics	Transient Characteristics of Charging Effects due to E-beam Irradiation: A Method of Charging Balance Mode
Trapped Electrons	Trapped Electron Environments of the Outer Planets
tube	Preventing Electrostatic Discharge in the Mars 2020 PIXL X-Ray Tube
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UNCOPUOS	Guidelines for Space Weather Research and Operation discussed in Space Weather Expert Group (SWEG) in UNCOPUOS /LTS WG
US Round-Robin Experiment on Plasma Propagation Speed	Arc Plasma Propagation and Arc Current Profiles
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vacuum arcing	High-fidelity Multi-Length Scale Modeling of Spacecraft Charging in GEO Orbit
Volume resistivity	P-C-13: Charging Characteristics of Electron Irradiated Polyimide Film under Cryogenic Temperature
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wake	P-C-12: Numerical Study on Plasma Disturbance near a Low-Earth Orbit Satellite
Wake Shaping	P-A-4*: Low Earth Orbit Plasma Wake Shaping and Applications to On-Orbit Proximity Operations
white paint	Conductivity of Thermal Control White Paints as a Function of Temperature and Surface Voltage
Wi-Fi	P-B-6: Wireless Antenna Detection of Electrostatic Discharge Events
wire harness	Analysis of Charge Accumulation Phenomena by Physicochemical Analysis for Fluorinated Polymer Films Irradiated by Proton
worst case	Spacecraft Potential Estimation in Worst Case Environment
worst case environments	P-C-37: Testing Materials under Electron Spectra Representative of GEO Worst-case Environments for Surface Charging
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x-ray	Preventing Electrostatic Discharge in the Mars 2020 PIXL X-Ray Tube

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