SCTC2018: THE 15TH SPACECRAFT CHARGING TECHNOLOGY CONFERENCE
PROGRAM FOR THURSDAY, JUNE 28TH
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09:00-10:15 Session 15: Theory, Modeling and Computer Simulations (1)
Location: Convention Hall
09:00
Modeling Surface Charging for NASA's Europa Clipper Mission
09:25
High-fidelity Multi-Length Scale Modeling of Spacecraft Charging in GEO Orbit
09:50
Advanced Numerical Schemes Implemented in SPIS to Improve the Accuracy of the Description of the Dense Cold and Drifting Plasma Populations
10:15-10:30Coffee Break
10:30-11:45 Session 16: Theory, Modeling and Computer Simulations (2)
Location: Convention Hall
10:30
Impact of Miniaturized Fixed-bias Multi-Needle Langmuir Probes on CubeSats
10:55
Simulation of the Electrostatic Environment of the Magnetospheric Multiscale Mission
11:20
Numerical Simulation of Spacecraft Charging Processes in Time-varying Plasma Environment
11:45-12:45Lunch Break
12:45-14:45 Session 17: Poster Session C
12:45
P-C-1: Simulation and Analysis of the SMILE Charging using SPIS
12:45
P-C-2: Spacecraft Surface Charging Simulation based on 3D Electrostatic PIC Model
12:45
P-C-3: Simulations of Non-ideal Effects In Langmuir Probe Measurements
12:45
P-C-4*: Simulations of the Rosetta Spacecraft Interaction with Comet Plasma
12:45
P-C-5: Improvement of the Spacecraft-Plasma Interaction Software (SPIS) with a New Versatile Architecture and Enhanced Modeling Capabilities for Electric Propulsion
12:45
P-C-6: (Moved to Oral Session 15)
12:45
P-C-7: Wake Formation behind Small Satellites
12:45
P-C-8: Differential Charging Estimation of Spacecraft in Single and Double Maxwellian Plasma Environment
12:45
P-C-9: Current Status of MUSCAT (Multi-Utility Spacecraft Charging analysis tools)
12:45
P-C-10: Particle Simulation Analysis of Spacecraft Charging Processes in Plasma Wave Environment
12:45
P-C-11: Numerical Study on the Plasma Disturbance an Charging Processes by Booms of an Ionospheric Rocket
12:45
P-C-12: Numerical Study on Plasma Disturbance near a Low-Earth Orbit Satellite
12:45
P-C-13: Charging Characteristics of Electron Irradiated Polyimide Film under Cryogenic Temperature
12:45
P-C-14: The Secondary Electron Emission Properties and the Influence on Charging Potentials
12:45
P-C-15: A Consideration of Degradation of Polymeric Materials in Sub-Low Earth Orbit Space Environment
12:45
P-C-16: Development of a Pulsed Supersonic Valve Aimed for Martian Atmospheric Simulation
12:45
P-C-17*: On the Use of a Detailed Electron Emission Model for Spacecraft Charging at Low Energy
12:45
P-C-18: Modification of Charge Body Migration in LDPE as a Result of Electron Radiation Exposure.
12:45
P-C-19: Effect of Plume Interaction with Spacecraft Materials on Electron Emission Properties and Electrical Characteristics
12:45
P-C-20: Dielectric Charging Mechanisms Involved in the Non-typical Electron Emission Yield Observed for Thin Dielectric Layers
12:45
P-C-21: Secondary Electron Yield Measurements of Carbon Nanotube Forests: Dependence on Morphology and Substrate
12:45
P-C-22: Charging Analysis with Changing the Satellite Surface Material Property due to Space Environment
12:45
P-C-23: Construction of Measurement System for Carrier Mobility in Insulating Materials for Spacecraft
12:45
P-C-24: Measurements of the Intrinsic Electron Yield of Highly Insulating Materials
12:45
P-C-25: Parameterization of Secondary and Backscattered Electron Yields for Spacecraft Charging
12:45
P-C-26: Electron Yield of Carbon-Composite Nanodielectric Material
12:45
P-C-27: Method for Touchless Determination of Electrostatic Potential and Material Composition for Spacecraft
12:45
P-C-28*: Remote Sensing of Spacecraft Electrostatic Potential using Secondary Electrons
12:45
P-C-29: Detailed Charging Analysis of Exposed KAPTON in GSAT-19
12:45
P-C-30: Concerning of the Spacecraft Charging for Space Debris Removal and Orbital Services
12:45
P-C-31*: An Efficient Hybrid Approach for the Reduction of Secondary Electron Yield
12:45
P-C-32: Dielectric Barriers for Arc Mitigation
12:45
P-C-33: Enabling Electron Beam Use in Tenuous Space Plasmas using Plasma Contactors: the Ion Emission Model
12:45
P-C-34: Dynamic Attenuation of Secondary Electrons Emission Yield of Fluorinated Polyimide Films
12:45
P-C-35: Significance of Shielding Kernel Selection for Spacecraft Charging Assessments
12:45
P-C-36: Improved Spacecraft Charging Roadmaps Developed to Support User Community Needs
12:45
P-C-37: Testing Materials under Electron Spectra Representative of GEO Worst-case Environments for Surface Charging
14:45-16:25 Session 18: Material Properties (1)
Location: Convention Hall
14:45
The Suppression of Spacecraft Charging based on Nanographene Composite
15:10
Worst-case Surface Charging: On the Importance of Measuring the Electron Emission Yield under Representative Environmental Conditions
15:35
Electrical Ageing of Polymers under Space Radiation Environment
16:00
Analysis of Charge Accumulation Phenomena by Physicochemical Analysis for Fluorinated Polymer Films Irradiated by Proton
16:25-16:50Coffee Break
16:50-18:30 Session 19: Material Properties (2)
Location: Convention Hall
16:50
Radiation-induced Conductivity in Kapton-like Polymers Featuring Conductivity Rising with Accumulating Dose
17:15
Conductivity of Thermal Control White Paints as a Function of Temperature and Surface Voltage
17:40
Time Evolved Constant Voltage Conductivity Measurements of Common Spaceborn Polymeric Materials
18:05
Spacecraft Charging Material Properties Database