Programme Content

Home , Cold gas thruster, Colloid thruster, Gridded ion thruster, Ion thruster, Pulsed plasma thruster, Vacuum arc thruster

Programme Content

Contact

Dr. Alexander Reissner General Chair ENPULSION → [email protected]

Dr. Carsten Scharlemann Overview 04 Chair of Technical Committee Fachhochschule Wiener Neustadt GmbH → [email protected]

Katrin Fangl Chair of Organizing Committee FOTEC Forschungs- und Technologietransfer GmbH Monday 10 → [email protected]

Tuesday 20

Where am I? Wednesday 24 To quickly find your sheduled talk, use Acrobat's "Find" tool.

1 Go to Menu: Edit → Find 2 Type your last name and it will appear highlighted in the document Thursday 34 Shortcut Windows ctrl + F Mac cmd + F

Friday 42 4 IEPC19 Programme Shedule / Floorplan 5

Monday 16 Tuesday 17 Wednesday 18 Thursday 19 Friday 20 Overview Plenary Lecture Paralell Sessions Paralell Sessions Paralell Sessions Paralell Sessions Welcome Speech / Raised Ground Floor David C. Byers Exhibition 09:00 Memorial Panel

Plenary Lecture Agencies 10.00

Plenary Lecture Conference Tour Industry Melk Abbey 11.00

Lunch / Lunch Lunch / Postersession Arkadenhof Postersession

12.00 Arkadenhof Arkadenhof

ERPS Technical Visits Meeting Vineyard Visit

13.00 Location

Plenary Lecture 13.30 LEO Paralell Plenary Plenary Lecture Sessions Lecture BepiColombo European

14.00 National Agencies Lower Level Sessions Seminraraum 8 Paralell Sessions Paralell Sessions Paralell Sessions Seminraraum 7 Hörsaal 6

15.00 Hörsaal 5

Hörsaal 3 Hörsaal 2 Seminraraum 6 16.00 Seminraraum 5 Seminraraum 4 Audimax 17.00

Gala Dinner Rathaus 18.00 19.00 20.00 21.00 6 IEPC19 Programme Poster Session 7 Monday 16 Thursday 19 Overview A109 A134 A250 A399 A489 A674 A803 A857 Heat Trnsfer Simulation Development of the Osaka A 3D Hybrid-IFE-PIC-MCC Frequency-time structure The Effect of Plasma Ion 2D (axial-azimuthal) Probe study on ion Molecular Dynamics in Radio-Frequency Ion Institute of Technology 2nd model for the discharge and mathematical models Current on the Acceleration Particle-In-Cell benchmark beam and backflow for Simulations of Nanodroplet Thruster PROITERES Nano-Satellite chamber simulation of ion of SPT emission in the of Field Reversed Configu- for ExB discharges different electric propulsion Break-up for Ionic Liquid V. Abgaryan with High-Power Electro- thrusters radio-frequency range ration Plasmoid T. Charoy technologies Electrospray Thrusters thermal Pulsed Plasma Y. Cao A. Plokhikh X. Sun V. Hugonnaud Y. Takao Thrusters for Powered A117 A697 Flight Non-preheated Hollow A256 A414 A490 Experiment Study on the A807 A866 H. Tahara Cathode for Hall Thrusters 2D Particle-in-Cell Numerical Investigation A PIC/MCC simulation on Property of 10cm ECR Combined optical emission Basic Characteristics of O. Petrenko Simulation of Current of Ignition in a Novel the initial ignition stage of a Ion Source Operating on and laser absorption Plasma Thruster using ICR A135 Characteristics in Three- Positron-Catalyzed Fusion 20mN Hall thruster Different Wave Radiation spectroscopy of Xenon Heating in Sheet Plasma Research of Debris Grid Ion Optics Propulsion Concept Mode gridded ion thruster A125 J. Yizhou A. Tonegawa Removal Systems by A. Sun L. Brieda Z. Hu R. Kozakov Analysis and test on Electric Propulsion and A509 A869 magnetic field for hall Development of the 4th A269 A416 A707 A809 thruster based on perma- PROITERES Nano-Satellite Experimental study of A Cylindrical Hall Thruster nent magnetic for Its Practical Space Evaluation of Coaxial 1-D PIC Model of a plasma parameters and Full-particle PIC/MCC Experimental Evaluation of for Mars Air Propulsion J. Hu Experiments at Osaka Short-pulse Laser-assisted Magnetically Enhanced quantitative analysis of numerical simulation of 2 the Micro Water Thruster Y. Nakayama Institute of Technology Pulsed Plasma Thrusters Plasma Thruster discharge instabilities in cm ECRIT ion source Recovering Waste Heat of a 500W Hall effect thruster Spacecraft A130 H. Tahara K. Sato M. Minute X. Xia A919 V. Desangles K. Nishii Performance Charac- Investigation of Electron teristics of High-Power A162 A286 A436 A716 Yield in a Ferrite Core RF A568 A812 Steady-State MPD Thrusters Studies on Helicon Plasma Investigation of Antenna Dynamic Acceleration Study of the electron Cathode to be Used in with Divergent and Cusp Thruster and Measurement Current and Regime Region Sizing and the Metallic Vapor Thruster anomalous transport in a Development of Microwave Plasma Thrusters Magnetic Fields Using Methods Transition in Electrodeless Impact on Breathing Mode using Field-emitted Hall effect thruster using a Discharge Ion Engine M. Celik Permanent Magnets for Inductive Plasma Gener- Oscillations Electron Bombardments 2D multi-fluid simulation with Variable Magnetic D. Kuwahara In-Space Propulsion ators J. Little P.-Y. Chang C. Gonzalez Field by Mover Permanent H. Tahara R. Georg Magnets to Axial and Radial A186 Directions A438 A570 A763 Design of Modular, High A131 A316 Y. Takao Efficient Anode Power Study of two-stage pulsed Development of a 200 W Particle-in-cell numerical Performance Character- Supply for Low Power Hall Experimental study on 25w plasma thruster with special Class Hall Thruster for an simulations of an helicon A813 istics and Interior Plasma Thrusters pulsed plasma thruster propellant combined ion Active Debris Removal double-layer thruster Phenomena of High-Power electric propulsion system liquid and resin manufac- System Integrated simulation S. Deshpande R. Miranda and High-Specific-Impulse X. Chen tured by 3D printer N. Yamamoto solutions for the plasma Hall Thrusters for In-Space and transversal physics in J. Saiki A764 Propulsion A194 electric propulsion systems A334 A587 Analysis of Erosion of Plas- H. Tahara A Thrust Balance for the M. Kubecka MINOTOR ECR Thruster Low frequency ionization A440 Fluid simulation of low ma Thrusters for Brazilian oscillation model with frequency oscillations in Space Missions Through S. Scharmann High Power Laser Powered A132 azimuthal dimension in a Propulsion Hall thrusters Numerical Simulations A814 Study on Low-Power Hall thruster K. Mori A. Rostek L. Braga Line-Integrated Barium Water-Cooled and A201 J. Bak Laser Absorption Spectros- Anode-Radiation-Cooled DC Design and Construction of copy Along Cathode Axis A636 A799 Arcjet Thrusters Using HAN a Rotating Magnetic Field, A483 A335 N. Wirgau and Water Propellants with Field-Reversed Configura- Numerical Simulations of Study on the Influences of Thermal analysis of Special Vaporing Systems tion (RMF-FRC) Thruster Feasibility study of a Capacitively Coupled RF Magnetic Field Configura- diode-laser coupled sublimable substance as tion on TAL Hall Thruster fiber-tip heat source A821 H. Tahara C. Sercel Micro-Thruster an alternative propellant to A. Popoli Discharge Chamber Plasma for high-temperature Development of microwave xenon in ion thrusters Characteristics generation discharge ion engine with A133 A231 M. Adachi C. Liu T. Matsuo mover permanent magnets Development of Longterm testing and A486 for changing a magnetic Commercially-Available evaluation of the vacuum Characteristics of laser field A350 A641 A800 Electrothermal Pulsed arc thruster system using sustained plasma using Y. Takao Plasma Thruster Systems multi-element cathodes Overview of SITAEL Electric argon and methane for on Design and test of Current Tests of the for Powered Flight of Micro/ Propulsion Developments board laser-based thruster 1cm-class RF Ion Micro Miniature Gallium Field M. Kuehn A835 Nano-Satellites at Osaka T. Misuri M. Matsui Propulsion System for Taiji Emission Electric Propulsion Institute of Technology Program in Space Thruster Computer Modeling of Non-Emission Electron H. Tahara J. He M. Xu Source with High Frequency Ionization S. Roshanpour MONDAY

Areas

 Physics and Fundamental Studies  Analytical Modeling  Numerical Simulations and Validation Against Experimental and/or Flight Test Data  Laboratory and Flight Testing  Diagnostics  Lifetime Characterization and Reliability  Mission Analysis  Systems Analysis  Development  Flight Experience  Other 10 IEPC19 Programme Monday 11

Material Technology Field Emission / Hall Thrusters 1 Hall Thrusters 2 Ion Thrusters Pulsed Plasma Commercial Global Innovative Cathodes, Gimbals Colloid Thrusters Thrusters Propulsion Needs Strategic Invests Concepts

HS6 SR5 SR6 SR7 HS5 SR4 HS2 SR8 HS3

Wecome Speech Audimax 09.00

David C. Byers Memorial Panel Audimax 09.30

Plenary Lecture Audimax Monday Agencies 10.00

Plenary Lecture Audimax Industry 11.00

Lunch Break & Poster Session 12.00

Plenary Lecture Audimax European National Agencies 14.00

A299  A149  A129  A532  A154  A184  A303  A189  A202  The Effect of Neutral Gas Development of Hybrid Data-Driven and Spatiotemporally Three-Dimensional Parti- The Modular Micro-Cathode Arc Versatile Xenon Flow Controller Activities of the H2020 Strategic Performance Scaling of Injection in the Keeper Ionic Liquid Electrospray Physics-Based Model for Resolved Ion Velocity cle Simulations of Electron Thruster for Extended Hall Effect Thruster Research Cluster on Space Drag-Modulated Plasma Orifice of a 25-A class Thrusters with a Massive Plasma Turbulence in a Distribution Measure- Extraction for a Miniature S. Hurley Power Range Electric Propulsion (2015-2019) Aerocapture Hollow Cathode Emitter Array for Higher Hall Effect Thruster ments in the 12.5 kW Microwave Discharge G. Lenguito J. Lopez Reig C. Kelly 14.00 S. Hall Thrust Density B. Jorns HERMeS Hall Thruster Neutralizer Using Water as Y. Takao V. Chaplin the Propellant Y. Sato

A300  A173  A147  A531  A309  A185  A505  A602  A254  The Role of Neutral Laboratory Demonstration Modular Comprehensive Ion Velocity Measure- Lifetime Evaluation of A Performance Comparison of New Propellant Approval at Evolution and Characteristics of Fluid-kinetic propulsive magnetic Pressure Due to Anode Ge- of a Staging System for Modeling of Plasma ments in the Magnetically Microwave Discharge solid Propellants in a Surface Arc Apollo Fusion Inc.—Activities to the Use of Electric Propulsion for nozzle model in the fully-magnet- ometry in Hollow Cathode Electrospray Thrusters Behavior in Hall Thrusters Shielded Miniature Hall Neutralizer using Thruster: Sulfur and Teflon Support Industry and Regulatory Low Earth Orbit Satellites ized limit Mode Transitions O. Jia-Richards T. Andreussi Thruster (MaSMi) Using Numerical Analysis S. Shimhanda Approval of New Propellant D. Lev M. Merino 14.15 S. Hall Laser-Induced Fluores- N. Hiorike M. Haverty cence V. Chaplin

A406  A225  A204  A513  A218  A273  A721  A711  A420  Development of a Colloid Micro-Thruster Model for the Increase in Charge Exchange Numerical study of A Coupled-inductive Energy Development of an additively The Importance of Electric Theoretical scaling laws for Diamond-Based Cold (CMT) Component Thruster Efficiency from Collision in the Plume of microwave discharge ion Storage Power Processing Unit manufactured mass, volume Propulsion to Future Exploration water-vapor propellant thrusters Cathode for Space Development Testing Cross-Channel Coupling a 200 W Laboratory Hall thruster µ10 for Micro-cathode Arc Thruster and cost optimised fuel tank of the Solar System A. Sheppard

14.30 Propulsion Applications Towards Meeting LISA in Nested Hall Thrusters Thruster Y. Yamashita J. Long for microsatellite propulsion J. Cassady I. M. Ahmed Rudwan Mission Requirements L. Su M. Baird systems MiniTank N. Demmons A. Bell 12 IEPC19 Programme Monday 13

HS6 SR5 SR6 SR7 HS5 SR4 HS2 SR8 HS3

A557  A372  A220  A868  A556  A456  A753  A439  Development of a Pure Ionic Electrospray Study on the Influence Performance Improvement Performance Evaluation and Progress in Automated System Application of Solar Electric Numerical study on a conical Microwave Discharge Extractor Design of Electron Conduction and Testing of a Micro- Development of Air Bearing Design by Evolutionary Algo- Propulsion in the Emerging shaped target for Laser Fusion Cathode for a 200 W Class Optimization Utilizing Paths on the Ignition wave ECR Neutraliser for a Thrust Measurement System of rithms Satellite Servicing Industry Rocket 14.45 Hall Thruster Additive Manufacturing Process of Hall Thruster Gridded Ion Thruster Surface Arc Thruster M. Ehresmann M. Glogowski T. Yamamura T. Morishita R. Antypas W. Li U. Khan K. Hiraka

A629  A277  A459  A276  A706  A616  A826  A778  A553  Development of a C12A7 The Effect of Ionic Magnetic Circuit Experimental Investiga- Two-Dimensional Development of Pulsed Plasma HEMPT-Strategy to address Spacecraft perspective trends Local Plasma Flow Coupling Electride Hollow Cathode Liquid Composition on Optimization for Hall tion of the Implications Particle-in-cell Simulation Thruster for a Pico-Satellite current and future Space Market and their propulsion systems with Plasma-wave Interaction in Monday and Joint Operation with Ion Electrospray Thruster Thrusters Design of Nesting Multiple Hall of 10 cm Microwave M. Sammut E. Bosch A. Sizovi Helicon Plasma Thrusters 15.00 Plasma Thrusters Performance T. Andreussi Thruster Channels Neutralizer B. Tian C. Drobny C. Miller S. Cusson Y. Fu

A644  A284  A470  A288  A272  A899  A212  A780  A717  Comparison of the thermi- Micro-Newton Electros- Theoretical Models of EP system development Hybrid-PIC Simulation of Filament-fed Pulsed Plasma The Benefits of Continued Compatibility of electric Validation of an Equivalent Circuit onic emission properties pray Thrusters for China’s Suppression of Instabil- and functional validation Back-sputtered Carbon Thruster (FPPT) for Small Advances in the Propulsive propulsion and spacecraft: Model for Rotating Magnetic Field of LaB6 and C12A7 Space-Borne Gravitational ities in Hall Thruster by tests for the Electra GEO Transport in electric Satellites Capability of the Electric GEO general requirements Field-Reversed Configuration

15.15 N. G. Kottke Wave Detection Mission Shear of Magnetic Field satellite propulsion test facility D. Carroll Communications Satellite E. Tverdohlebova Thrusters (Tian Qin) A. Kapulkin V. Garcia H. Zheng J. Trescott J. Woods P. Song

A482  A344  A278  A142  A302  A657  A210  A876  Development of High Characterisation of A Comparison of Possible Hall thrusters develop- EMC considerations for RIT A Vacuum Arc Ion Thruster for EP orbit raising: environmental Propulsion subsystem for a stand Current LaB6 hollow electrospray microemit- Mechanisms for Facility ment at Exotrail: pres- engines based on 3D full- SmallSat Applications effects impact on satellites, alone interplanetary CubeSat Cathode ters fabricated by planar Effects on Hall Thruster entation and experimental wave field simulation of J. Kolbeck modelling and challenges D. Feili

15.30 W. Yang and 3D photolithography Operation investigation electromagnetic emission B. Zitouni T. Henning T. Matlock A. Gurciullo of their RF coils T. Sommavilla

A695  A650  A306  A114  A496  A860  A883  A275  Featherweight Heaterless A Novel Variable Mode A comprehensive xenon Hall Thruster ST-25 Numerical simulation of Optical measurements of ablation More added value? – an investi- High power electric propulsion: Hollow Cathode Charac- Emitter for Electrospray collisional-radiative designed by Space plasma discharge in RF ion process of double-cylindrical gation on the commercial benefit MARS plus EUROPA - already terization Thrusters model of atomic and ionic Electric Thruster Systems thruster pulsed plasma thruster of different EP technologies for beyond 2025!

15.45 M. Mooney P. Wright excited levels for Hall (SETS) R. Rakhimov T. Inaba orbital propulsion instancing F. Jansen thruster O. Petrenko H2020´s GIESEPP Y.-F. Wang C. Dietz

A768  A223  A762  A791  A905  A421  A790  A607  A176   Evaluation of Iodine Direct Thrust Meas- Stationary Profiles and Performance Comparison Analytical and numerical Performance and Efficiency of Development of a 100 mN VENUS - Updates on Technologi- Effects of magnetic shielding on Compatible Hollow urement and Plume Axial Mode Oscillations of a 2 kW Hall Thruster simulation of Ring Cusp Electric Solid Propellant in a Horizontal Torsion Balance cal Mission Using IHET the performance of Multi-cusped Cathode Configurations Characterization of a in Hall Thruster with Heaterless Cathodes Discharge Chamber Pulsed Plasma Thruster B. Seifert D. Lev field thruster S. Thompson Porous Electrospray A. Smolyakov Mounted on the Outer F. Cannat M. Glascock P. Hu 16.00 Thruster Pole Piece and on the C. Ma Thruster Centerline T. Andreano

A802  A296  A846  A441  A367  A659  A413  A418  A243   Diagnostic analysis of a Experimental Validation of Proportional Thermal Development Status of Plasma characteristics Micro-cathode arc thruster Design and testing of a μN Electric Propulsion for Small Electric Propulsion Pointing 30 A heaterless hollow a Dielectric Electrospray Model for Hall Thrusters 6-kW-class Hall Thrusters in the backflow region of improvement by the second MPD - mN torsional thrust balance Satellites: A Case Study Mechanism EPPM for the cathode Emitter with a Directly with Magnetic Shielding at JAXA ion thruster plumes using stage with wireless microwave power P. Lascombes Spacebus Neo Platform

16.15 A. Daykin-Iliopoulos Deposited Thin Film M. Porto I. Funaki kinetic and electron fluid K. Daniels transmission A. Derntl Electrode models K. Swar A. Kimber N. Nuwal 14 IEPC19 Programme Monday 15

HS6 SR5 SR6 SR7 HS5 SR4 HS2 SR8 HS3

A890  A471  A264  A342  A529  A662  A784  A373   Characterization of a Development and A thermo-mechanical Parametric study of Study of Ion Thruster Experimental Analysis of Cusped TIDBIT - Thruster In-Space Plasma Magneto-Shell Aerocap- Fixed-Volume Release Characterization of an analysis with the use of 1,5- and 2.5-kW Hall Backflow Characteristcs Magnetic Field Focusing on Diagnostics with Bus Integrated ture for Manned Mars Missions System for Initiating an Arc Ionic Liquid Electrospray tasks in a non-linear for- Thrusters with an external with Neutralization Using Vacuum Arc Thrusters Telemetry and Planetary Deep Space Discharge in a Heaterless Thruster with a Porous mulation for a low-thrust discharge zone Kinetic PIC-DSMC M. Laterza T. Matlock Orbiters Hollow Cathode Metal Blade Array thruster calculations A. Lovtsov D. Levinl J. Slough 16.30 R. Ham X. Liu during lifetime prediction with the SPT-50 thruster as an example O. Olshanskaya Monday A422  A522  A392  A473  A798  A211  A398   The development of the Performance of a Fully Laboratory tests of Parallel codes using An investigation of alternative Thrusters modelling, propellant Modeling, Simulation and Testing Integrated Thruster Unit Conventionally Machined 10.5kW Hall thruster with non-uniform meshes propellants for pulsed plasma choice and plume expansion: of a Magnetically Enhanced RF ITU100 and ITU140 Liquid-Ion Electrospray external layer and view factor model thrusters openPlumeEP capabilities Plasma Source for a High Power A. Zarakovskiy Thruster Operated in PIR A. Shashkov methods for particle in W. Y. L. Ling B. Zitouni Electromagnetic Thruster

16.45 M. Natisin cell-Monte Carlo collision X. Wen (PIC-MCC) simulation in ion thruster R. Pan

A881  A787  A681  A740  A565  A554  A123  A547   Harmonization of European Reconstructing Elec- Status of Research Performance of the Aurora Numerical simulation Ignition Capability of Pulsed Cryopumping Challenges of Electric Propulsion Activities Mechanisms for Electric trospray Plume Current Activities on Electric Low-Power Hall Effect of electrospray thruster Plasma Thruster with Green EP-Propellants in DLR’s Electric at the UCLA Plasma Space Propulsion Spatial Distributions using Propulsion at CIRA Thruster extraction for highly Liquid Propellant Propulsion Test Facility Propulsion Laboratory 17.00 M. Toso Computed Tomography V. Salvatore J. Sommerville conductive propellants J. Aoyagi A. Neumanni R. Wirz D. Courtney H. Huh

A289  A794  A241  A910  A612  A898  A796  A549   Development and Investigation of Electros- PPS®X00 Hall Thruster Performance, Stability, Elegant Approach for Micro-Cathode Matrix Arc Development of Propulsion Possible electric propulsion Qualification of an Electric pray Plume Composition Development Status at and Wear Characteriza- solving the Conservation Thrusters- A Modified Approach Testing and Integration Facilities schemes based on a combination Propulsion Thruster during Voltage Transients Safran tion of a Sub-Kilowatt Hall Laws in Global Modelling to Micro-Cathode Arc Thrusters at Canon Electronics of RF and DC discharges

17.15 Orientation Mechanism for E. Petro J. Vaudolon Thruster of Radio-Frequency Ion K. Daniels K. Masuyama I. Zadiriev the Electra GEO satellite H. Kamhawi Thrusters V. Garcia A. Reeh

A840  A884  A655  A216  A699  A656  A564   Research and develop- An energy-dispersive SITAEL HT100 Thruster, Performance of a Three-dimensional Inter-Laboratory Comparison: Experimental Study of Traveling ment of radio-frequency mass spectrometer for Full Ground Qualification 100-Watt Radial Scaled simulation of ion Tests of a single thruster in Wave Plasma Acceleration and cathode-neutralizer electrospray propulsion T. Misuri Thruster with Anode Layer thruster plume-spacecraft two different facilities, on two Optimization of Magnetic Field

17.30 P. Smirnov diagnostics A. Olano Garcia interaction using EX-PWS different thrust balances Structure for Electrodeless RF N. Ford H. Zheng F. G. Hey Plasma Thruster Y. Oshio

A477  A825  A527  A491  A653  A572   CNT-based cold electron Development status of Design and performance Studying the formation University of Michigan’s The Transport Character of the source for space applica- SITAEL’s 20kW class Hall test of the BEHT200 low and neutralization of an Upgraded Large Vacuum Test Field Reversed Configuration tions on nano-satellites thruster power hall thruster ion thruster plume with Facility Plasmoid in the Field Reversed 17.45 P. Laufer T. Andreussi Y. Hu EP2PLUS E. Viges Propulsion Thruster J. Perales-Díaz L. Lijuan 16 IEPC19 Programme Monday 17

HS6 SR5 SR6 SR7 HS5 SR4 HS2 SR8 HS3

A885  A410  A804  A321  A847  A766  SITAEL’S HT400 Mechanism Behind the Theoretical and Experi- Experimental Study on Ignition Improved Pumping Speed of Design of an Experiment for Com- Hall-Effect Thruster for Dependence of Thrust mental assessment of Ion Reliability of Pulsed Plasma Custom Cryopumps for Electric pression and Nozzle Expansion of Constellation Applications on Facility Backpressure Extraction phenomena Thrusters Propulsion Vacuum Facility a Field-Reversed Configuration T. Misuri and Implications on the M. Mallon X. Liu M. Crofton for Advanced Space Propulsion

18.00 Operation of the SPT-140 P. Turchi Onboard the Psyche Mission I. Mikellides

A506  A714  A834  A536  A785   Monday Electric Propulsion Impact of Facility Development of a 3D ion The study on the lifetime of the Electromagnetic Propulsion Using Activities at Apollo Fusion Pressure on the Wear of optics modelling code micro cathode arc thruster Non-Ionized Dipole Gases Inc.—Design, Develop- the NASA HERMeS Hall S. Centola J. Geng M. Micci ment, and Qualification of Thruster 18.15 a Low Power Hall Thruster J. Frieman Subsystem J. Delgado

A193  A630  A854  A661  A848   The 12.5 kW Hall Effect Data-driven Models for Neutral Density Simulation Influence of Insulator Geometry Low-Field Mode Transitions in a Rocket with Magnetic the Effects of Background in the Grid Region of Ion on Vacuum Arc Thruster Lifetime Spiral-Antenna Helicon Thruster Shielding (HERMeS) Pressure on the Operation Thrusters using the ffx Ion M. Laterza J. Little 18.30 R. Hofer of Hall Thrusters Optics Code M. Byrne J. Williams

A266  A664  A169  A852   A 30-kW Class Magneti- Test Results of ExoTerra's Predicting Pulsed Plasma Laboratory demonstration of cally Shielded Nested Hall Halo Electric Propulsion Thruster Performance with Deep a bidirectional helicon plasma

18.45 Thruster Module Recurrent Networks thruster for space debris removal S. Cusson M. Vanwoerkom P. Shaw K. Takahashi

A713  A893  A933   Variation in Ion Pulsed Plasma Acceleration Lodine as propellant for electric Acceleration Character- Modeling in Detonation and propulsion: optical measurements istics of the HERMeS Hall Deflagration Modes of I density and temperature,

19.00 Thruster during Magnetic K. Polzin comparisons to a global model Optimization F. Marmuse W. Huang

Session End TUESDAY

Areas

Material Technology Field Emission / Hall Thrusters 1 Hall Thrusters 2 Ion Thrusters Pulsed Plasma Innovative Power Processing Thruster Cathodes, Gimbals Colloid Thrusters Thrusters Concepts Developments Concepts

HS6 SR5 SR6 SR7 HS5 SR4 HS3 SR8 HS2

A628  A213  A492  A904  A355   A108   A361  A110  A242  Experimental characterization of Quantitative mapping of the Development of a 5kW Class SITAEL’s HT5k LL Magnetically- Physics Principles for Opti- Analysis of Distributed Directed-Energy Hight-efficiency Digital Filtering of Electric the attachment length in orificed mechanisms affecting electros- Hall Thruster Shielded Hall Thruster Tests mization of HEMP-thruster Energy Release Charac- Propulsion Architecture discharge power supply Thruster Time Domain hollow cathodes pray thruster lifetime C. Mullins T. Andreussi using PIC simulations teristics in an Ablative for Deep-Space Missions for engine system with Radiated Emissions

09:00 P.-Y. Taunay A. Collins P. N. Maya Pulsed Plasma Thruster with Characteristic Velo- Hall Thruster N. Rongione L. Yang cities of Order 100 km/s O. Petrenko J. Polk

A663  A368  A140  A879  A504   A457   A458  A187  A521  Two-Photon Absorption Laser Resolving electrospray emission Development of a 1.5KW High SITAEL’s Magnetically Shielded Key factors affecting the Preparation of space Hybrid Electric Propulsion Study of Operation of Direct thrust measurement Induce Fluorescence (TALIF) of modes using high-speed current Specific Impulse Magnetic 20 kW Hall Thruster Tests parameters of inductive RF experiment to study System on the Basis of Power and Propulsion of a vacuum arc thruster Neutral Xenon Density in a Barium measurements Shielded Hall Thruster T. Andreussi ion thruster in continuous ionosphere using pulsed SPT and PPT System based on Closed J. Jarrige Oxide Hollow Cathode Plume N. Uchizono A. Mishra and pulsed operating plasma injectors with M. Kazeev Brayton Cycle Power 09.15 T. Wegner regime increased power aboard Conversion Unit and E. Kralkina the ISS Electric Propulsion A. Bogatyi A. V. Karevsky

A689  A571  A274  A591  A678   A497   A508  A270  A595  Time-Resolved Electron Density Spatially-Resolved Electrospray High Throughput 1.5 kW Preliminary tests of HIKHET Global model of a Investigation on the Optimization of Electric Electric Propulsion Mechanically amplified and Temperature Measurements Plume Current and Mass Flux Hall Thruster for Satcoms laboratory model at IPPLM magnetized ion thruster Discharge Arc Behaviour Propulsion System Param- Mission Design with milli-Newton thrust Tuesday in a Hollow Cathode Discharge Measurements and Analysis S. Zurbach J. Kurzyna with xenon and iodine of an Asymmetric eters of LEO Spacecrafts Minimal Solar Cells balance for RF-thrusters

09.30 by Cavity Enhanced Thomson A. Thuppul R. Lucken Electrodes Pulsed M. Kazeev Radiation Degradation M. Wijnen Scattering Plasma Thruster A. Starchenko A. Friss Z. Zhang

A760  A892  A901  A735  A831  A533   A424  A190  A715  5-100 A LaB6 Hollow Cathodes Characterization of Electrospray Development of the High Voltage Preliminary Tests of UK90 Investigation on Plume and current-volt- Crosscutting High High Efficiency Auto Development of the for High-Power Hall Thrusters Thruster Electrode Overspray Hall Accelerator Propulsion Hall Thruster with Internal Alternative Propellants for age characterization of Apogee Refueling Orbital Resonant Converter SPACE Lab Thrust Stand G. Becatti and Backspray System Hollow Cathode Gridded Ion Engines the micro-Cathode Arc Navigator (CHARON) for Anode Power Supply for Millinewton Thrust

09.45 C. Marrese-Reading H. Kamhawi U. Kokal N. Fazio Thruster Active Debris Removal Design, Development Measurement Y. Qin J. Slough Testing P. Thoreau M. Richards

A427  A909  A282  A343  A862   A576   A462  A280  A578  Mode Transition in a LaB6 Hollow Microfluidic and materials Overview of the Ascendant Effects of Thrust Noise on Integrated Vlasov-Fully Temporal and Spatial Ion Concept Study Deep Space Power Self-calibration Laser Cathode for Electric Propulsion improvements in the ion Sub-kW Transcelestial Electric Drag-Free and Attitude Kinetic PIC Simulations of Velocity Distributions of of Air-breathing Processing Unit for the Induced Fluorescence Systems for Small Satellites Electrospray Propulsion System Propulsion System (ASTRAEUS) Control System Plasma Plumes a Short-pulse Coaxial HeliconThrust In an Psyche Mission technic in Electric Propul-

10.00 G.-C. Potrivitu B. Kristinsson R. Conversano K. Cui C. Cui Laser-assisted Pulsed Ultra-low-Orbit S. Malone sion plasma diagnosing Plasma Thruster Q. Y. Ren X. Yang T. Mikami

A428  A283  A377  A882   A476   A485  A346  A863  Systematic Testing of Improved Development Acceptance Mini-CHT powered Formation Influence of Hollow Cath- PETRUS 2.0 PPT and Ultra-low- orbit Space- Designing, Manufacturing Laser ablation plasma Designs of Miniaturized LaB6 Testing of the Thruster Compo- Flying Mission for Magnetic ode design parameters its CubeSat-size PPU: craft Long Term Sustained and Testing of Power diagnostics for electro- Hollow Cathodes for Electric nent of the Ascendant Sub-kW Reconnection Research in Space on Ring Cusp Discharge Testing and Characteri- H. Zhao Processing and Control static acceleration

10.15 Propulsion Systems for CubeSats Transcelestial Electric Propulsion J. Simmonds Chamber performances zation Unit for a 1.5 kW Hall A. Hamada and Small Satellites System (ASTRAEUS) F. Cannat C. Montag Effect Thruster G.-C. Potrivitu R. Conversano S. Neugodnikov

A369  A873  A651  A409  A623  Lithium Hollow Cathode for Development of a low power The Application of an Advanced Design and Implemen- Active Wave Injection a Very High Isp Interstellar HEMP Thruster EV0 Electric Propulsion System on tation of a High Voltage Diagnostic for Plasma Precursor Ion Thruster R. Heidemann the NASA Power and Propulsion Supply for Gridded Ion Dispersion Relation

10.30 D. Goebel Element (PPE) Thrusters using model- Measurements D. Herman based control algorithms S. Rojas Mata C. Roessler

A371  A878  A419  A538  High Current Hollow Cathode HT5k Development Status, REGULUS: Know-How Torsional Balance Thrust for the X3 100-kW Class Nested Future Activities and Market Acquired on Iodine Measurement Techniques

10.45 Hall Thruster Opportunities Propellant for Small RF Thrusters G. Becatti T. Andreussi D. Pavarin C. Cretel

Conference Tour 11.00 WEDNESDAY

Areas

Material Technology Field Emission / Hall Thrusters 1 Hall Thrusters 2 Ion Thrusters Resistojets/ Innovative Power Processing Thruster Cathodes, Gimbals Colloid Thrusters Arcjets Concepts Developments Concepts

HS6 SR5 SR6 SR7 HS5 SR4 HS3 SR8 HS2

A782  A139  A906  A156  A356  A224  A158  A423  A232  Recent Advances in Low-Current Dual-Axis Torsional Thrust Qualification Status of the PPS® Code-to-Code Verification of T7 thruster design and Electrostatic Probe Optimum design for RF Power Processing for a Electromagnetic-PIC Hollow Cathodes at SITAEL Stand for Simultaneous Direct 5000 Hall Thruster Unit Stochastic Models for Electric performance Investigation of Very Low the drive-coil of a 500J VASIMR® System simulation of an ECR D. Pedrini Measurement of Thrust and O. Duchemin Propulsion Plume Simulation J. Perez Luna Power Arcjet VELARC inductive pulsed plasma J. Squire plasma thruster

09:00 Mass Loss S. Araki in IRS and ESA-ESTEC thruster and its numerical J. C. Porto M. Gilpin Facilities evaluation J. Skalden B. Che

A207  A226  A673  A157  A688  A122  A191  A474  A415  Tests of an iodine-fed rf-neu- Investigations into multiple Qualification status of the Unified Framework for Hall-Effect T5 Performance, Indus- An Efficient Ionization Effects of Collisional-Ra- Development of a Numerical Model of a tralizer emission sites in porous EP system for Heinrich Hertz Thruster, Plume, and Spacecraft trialisation and Future Method for Pressure Up diative Processes with full bridge series Magnetically Enhanced P. Dietz electrospray thrusters satellite (H2Sat) Charging Models to Assess Applications To Thousands of Pascals Relative Drift in Electric resonant radio-frequency Plasma Thruster

09.15 C. Tacon S. Ciaralli Spacecraft Integration P. Randall L. Chang Propulsion Devices generator for optimized M. Magarotto S. Araki R. J. Abrantes RIT operation J. E. Junker

A896  A445  A599  A222  A360  A170  A248  A512  A426  Ariane Group 5A Neutralizer Development of a Retarding Development and Performance Long-term Scale Characteristics Testing of a 50,000-s, The Development and Electrocoalescence High Voltage Power Development of a PIC- qualification status Potential Analyser for Low Test of a 50 W-class Hall thruster of Low-frequency Oscillation of Lithium-fueled, Gridded Qualification of the STAR in Ultrasonic Electric Supply for T5 Gridded Ion FDTD code for modelling C. Altmann Density FEEP Thruster Beam D. Lee Hall Thrusters Ion Thruster Resistojet System for Propulsion system Thruster RF plasma discharge

09.30 Diagnostics L. Wei J. Brophy Telecommunications W. He M. Blaser R. Kalampattel N. S. Mühlich Applications F. Romei

A297  A566  A461  A235  A640  A786  A259  A567  A460  Performance Testing of a Two-dimensional plasma plume Design and preliminary testing Study of Xenon Wall Accommoda- HEMPT Ion Thruster A 17.8-GHz Ammonia Water as an Alternative Design and Manufactur- Simulations of magnetized Microwave ECR Neutralizer for density characterisation of the of a laboratory low power Hall tion Model and Background Flow Operation with Krypton Microwave Electrothermal Propellant for a Next ing of Control Unit for low plasma thruster plumes the X-EPT Gridded Ion Thruster IFM Nano Thruster Thruster During Hall Thruster Ground Test Propellant Thruster for CubeSats and Generation Plasma and medium power Hall F. Cichocki 09.45 for Telecoms Applications S. Keerl M. Panelli G. Ito A. Genovese Small Satellites Propulsion System Effect Thruster S. Reeve M. Micci A. Schwertheim S. Neugodnikov Wednesday A148  A260  A832  A263  A811  A393  A265  A575  A564  Improving EP device performance MEMS FEEP Thrusters – Minia- Preliminary design of a low-pow- Numerical Investigations of Development and testing Lifetime Investigations of Multifluid FRC Formation Development of High Investigation of the Circuit and lifetime with plasma-robust turised Liquid Metal Ion Source er Hall Thruster Background Pressure Effects and of the NPT30 ion iodine an Additively Manufac- Modeling with Relative Efficiency Power and Ablation Model for a surface architectures using Glass Capillaries C. Groll Channel Erosion in the SPT-140 thruster tured High-temperature Drift Corrected Collision- Processing Unit for Hall Vacuum Arc Thruster

10.00 C. Huerta M. Tajmar Hall Thruster for the Psyche J. Martínez Resistojet Heat Exchang- al-Radiative Processes Thruster S. Bai Mission er from Tantalum R. Lilly A. Tsybulnyk A. Lopez Ortega M. Robinson

A172  A362  A634  A247  A383  A403  A324  A584  A573  LaB6 hollow cathode work Development, Production, and Development and Characteri- Numerical Simulations of AFRL Development of 50 W Failure analysis of Numerical investigation Power Processing Unit Numerical Analysis of function enhancement: insight Testing of the IFM Nano FEEP zation of a Miniature Hall-Effect EP/TEMPEST experiment class RF gridded ion endurance tested 316L of “Detachment Cone” in Activities at Thales Alenia Plasma Acceleration into the chemical processes Thruster Thruster using Permanent using the Thermophysics Unified thruster stainless steel Super High the magnetic nozzle Space in Belgium Driven by Loop Coil in P. Guerrero T. Schönherr Magnets Research Framework (TURF) D. Q. Pham Tran Temperature Additive Z. Chen E. Bourguignon Electrodeless Thruster 10.15 N. Gondol L. Brieda Manufactured Resistojet Y. Yamakawa (STAR) C. Ogunlesi

A245  A675  A375  A237  A446  A631  A330  A696  A647  Plasma model and experimental The IFM Micro FEEP thruster: Miniaturized Cylindrical Hall Study on Feed System of Iodine Development Status of Effect of structure Numerical Simulations Flying Capacitor Optimization of electro- investigation of a hollow cathode a modular design for smallsat Thrusters Cusped Field Thruster Microwave-ion Thruster characteristics on of the Plasma Discharge Multilevel Converters thermal microwave plasma neutraliser propulsion J. Simmonds H. Liu M5 for Small and Micro start-up process of an in an Helicon Plasma for use in the ASTRAEUS thruster for nanosatellites 10.30 A. Gurciullo L. Grimaud Satellites Arcjet thruster Thruster Anode Power Supply S. Ivanov K. Zhu Y. Shen J. Zhou A. Barchowsky

A301  A686  A465  A285  A900  A560  A728  A666  Hollow cathode thermal model- The ESA Earth Observation Pro- Investigation of the possibility to Influence of plume magnetic field The Development and Research on Micro RAFAEL's Compact Power Nanosecond Pulsed ling and self-consistent plasma gramme activities for the design, develop competitive small power on discharge performance of Test of a Dual Mode Micro Impulse Measurement Supply Unit (PSU) for Micro-Plasma Thruster for solution: two step neutralization development and qualification of stationary plasma thruster (SPT) Hall thruster under internal and Microwave Gridded Ion Technology for Micro an Affordable Electric Small Satellites

10.45 modelling the mN-FEEP thruster V. Kim external cathode position studied Thruster for Orbit Raising Cathode Arc Thruster Propulsion System (EPS) N. Rogers P. Guerrero L. Massotti by particle-in-cell simulation and Attitude Keeping X. Liu D. Lev X.-F. Cao A. Vafabakhsh 26 IEPC19 Programme Wednesday 27

HS6 SR5 SR6 SR7 HS5 SR4 HS3 SR8 HS2

A331  A805  A836  A294  A652  A225  A590  A729  A795  An Axisymmetric Eulerian-Kinetic CLIMB: Exploration of the Van Overview of NASA’s Solar Electric EP plasma plume in orbit: Diag- Performance Testing of Development Progress Interaction of Droplets in Rafael's Power Process- Numerical Simulation and Solver for Simulation of Hollow Allen Belt by CubeSats Propulsion Project nostics and analysis correlation the X-EPT Microwave ECR of an Adaptable Deorbit Electrospray Plumes ing Unit (PPU) for Electric theoretical analysis of Cathodes C. Scharlemann P. Peterson J. Laube Gridded Ion Thruster for System for Satellite M. Davis Propulsion Systems Particle Acceleration in

11.00 A. R. Vazsonyi Telecoms Applications Constellations D. Lev Traveling Magnetic Field D. Hoffman J. Skalden Thruster H. S. Kumar

A452  A724  A779  A639  A143  A390  A633  A888  A609  A Plasma Model for Orificed Recent flight data of the IFM Development of low-power micro Coupling of an all-electric Development of the Performance Theory PIC/fluid/wave simu- AIRBUS DS PPU Discrete Boltzmann Hollow Cathodes Nano Thruster used for LEO orbit cylindrical hall thruster “SCHT-1” spacecraft with its plasma plume Miniature Xenon Ion and Development of a lations of the plasma qualification status for Modeling of Atmospheric raising and its environment Thruster with Hollow Resistojet Based Hybrid discharge in an ECR HET, GIT and New Space Pressure Plasma Jet

11.15 M. Panelli T. Ikeda D. Krejci S. Hess Cathode Operation Electro-Chemical Thruster plasma thruster Technologies J. Song S. Samples G. Coral A. Sánchez-Villar F. J. Pintó Marín

A914  A828  A702  A833  A558  A913  A818  Validation of a drift diffusion UWE-4: In-orbit characterization Development of BUSTLab Low Simulation of plasma plume Development of 5 Development of a High Effect of the initial model for a hollow cathode of the NanoFEEP propulsion Power Hall Thruster for Use at experiments with Hall Thrusters: kilo-watts electric Voltage Power Process electron distribution S. Gabriel system LEO Mini-Satellite Systems on-ground chamber effects on propulsion system on Unit for a CubeSat function in magnetic

11.30 A. Kramer U. Kokal measurements and extrapolation Satellite SJ-20 Electrospray Thruster nozzle expansions to in-flight situation G. Jun C. Ma S. Correyero Plaza P. Sarrailh

A781  A895  A856  A858  A754  A930  A744  A One-Dimensional model for LISA Colloid Microthruster Small Permanent Magnets Hall Thruster Plume and Spacecraft NEXT-C Flight Ion System 13kW Advanced Electric A 3D Numerical Study of Hollow Cathode Orifice lifetime Technology Development Plan Plasma Thruster Development Interaction Analysis by 3D Development Status Propulsion System Arcjet Thrusters: Effect of prediction and Progress for Micro and Nano Satellites Electrostatic Code for 4.5-kW- J. Fisher Power Processing Unit Electrode Configuration

11.45 F. Bosi J. Ziemer J. Ferreira Class Hall Thruster Development on Performance of Arcjet T. Muranaka E. Soendker thruster N. Hari Prasad Wednesday A627  A912  A937  Experimental investigations and High Power Ion Propulsion Research on a controlled performance optimisation of the System for the Double high voltage power supply Lunch Break Halo thruster Asteroid Redirection Test for Power Processing Unit 12.00 S. Masillo Mission Q. Kang J. Fisher

A464  Development of compact high efficiency RF generator for inductive 12.15 coupled plasma sources A. Surminskii

Plenary Lecture Audimax LEO 13.30

A783  A196  A336  A318  A668  A520  A174  A198  Numerical modeling and Droplets emission from FEEP and The research of the modified Coupled Simulation of Two-Di- The Analysis of Parameter Numerical Investigation Design and preliminary Electrodeless Helicon incoherent Thomson scattering colloids thrusters: modelling of SPT-70 thruster parameters and mensional Hybrid Hall Thruster Sensitivity of Electron of Micro-Cathodic Arc experiments of the Plasma Thruster Employing measurements of a 5A cathode droplets dynamics and interac- characteristics Models backstreaming failure Thruster Lifetime using prototype of a 500J Additional Electromagnetic

15.00 with LaB6 emitter tion with spacecraft body A. Markov R. Kawashima mode for 3-grid system ion the PIC-DEM Method inductive pulsed plasma Acceleration Method L. Garrigues M. Villemant thruster L. Brieda thruster T. Furukawa Y. Jia X. Li 28 IEPC19 Programme Wednesday 29

Material Technology Field Emission / Hall Thrusters 1 Hall Thrusters 2 Ion Thrusters Resistojets/ Innovative Thruster Cathodes, Gimbals Colloid Thrusters Arcjets Concepts Concepts

HS6 SR5 SR6 SR7 HS5 SR4 HS3 HS2

A865  A317  A660  A518  A680  A837  A178  A537  Comparisons between Particle Uncertainty Quantification of I2HET: Development of an Hybrid modeling of the Surface Modification of Pyro- Numerical Rebuilding of Very The Status of the VASIMR(R) An Experimental Study of Thrust Simulation using IAT Growth Electrospray Thruster Array Iodine-Fed Hall Effect Thruster anoumalous transport inside Hall lytic-Graphite Grids for an Ion Low Power Arcjet Thruster Engine Development Program Dependence on Magnetic Field Model and Plume Measurements Lifetime M. M. Saravia thrusters thruster VELARC in Test Facilities at IRS M. Carter in an Electrodeless Inductive 15.15 of LaB6 Hollow Cathode B. Jorns A. Alvarez Laguna Y. Matsunaga and ESA-ESTEC Plasma Accelerator K. Kubota P. P. Upadhyay A. Tatsuno

A874  A526  A838  A648  A722  A562  A583  A596  Fluid model of a Hollow Cathode Colloid Thruster Plume Simula- Simulation of an Adaptable Hall Multiscale Hybrid Modeling of Uncertainty Quantification of A Chemically Augmented Arcjet Advanced and nanostructured Development and Character- discharge tions Using a Particle-Particle Thruster Unconventional Hall Thrusters Modeled Electron Backstreaming Thruster with Exotic Propellants materials for electric propulsion ization of the Helicon Plasma

15.30 X. Chen Model N. Proulx M. Laterza Failure for the NEXT Ion Thruster M. Tsuchiya and small satellites Thruster Prototype HPT-03 J. Wang J. Yim I. Levchenko J. Navarro-Cavallé

A658  A530  A902  A358  A827  A703  A646  A608  Numerical and Experimental Effect of Aprotic + Protic Performance, Plume, Stability, The impact of the SPT-140D Endurance Testing of Iodine BIT-3 Effect of adding water to Operation and Performance of a XMET: Testing of an Argon/ Investigation of Different Heater Mixtures on Electrospray Droplet and Wear Characterization of parameters and lifetime RF Ion Propulsion System propellant of a DME arcjet Fully-Integrated ion Electrospray Xenon Microwave Electrothermal Designs for Lanthanum Hexabo- Fragmentation Three Alternate Magnetic Field characteristics change on its M. Tsay thruster Propulsion System Thruster

15.45 ride Hollow Cathodes D. Levin Topologies in the Hall Effect thermal mode T. Tachibana B. Kristinsson T. Baxter U. Kokal Rocket with Magnetic Shielding P. Chubov H. Kamhawi

A144   A830  A637  A281  A907  A742  A855  Porous Materials for Long Life Development of an Electrospray Characterisation and Plasma Simulations for the Modeling Ion Optics Erosion in Direct Inertial Electrostatic Performance improvement of a and High Performance Electric Source Model for Kinetic Plume Performance Comparison of a Assessment of Pole Erosion in the the NEXT Ion Thruster Using the Confinement Propulsion at Low magnetic nozzle helicon plasma Propulsion Modeling Low-Power Hall-Effect Thruster Magnetically Shielded Miniature CEX2D and CEX3D Codes Power Levels thruster G. Li E. Petro and an Advanced Cusp Field Hall Thruster (MaSMi) J. Polk M. Winter K. Takahashi 16.00 Thruster with Multiple Noble A. Lopez Ortega Gases M. Vaupel

A153   A559   A752  A364  A761  A867  Wednesday Development of Low-Volt- Study on Performance of Ionic Preliminary Evaluation of Particle-In-cell / fluid simulations Experimental demonstration Cubesat Test Platform for age-Driven Propellantless Liquid Electrospray Thruster Anode-Layer-Type Hall Thruster of a Hall effect thruster account- of thrust vectoring magnetic miniaturized electric propulsion Cathodes with High-Current in Atmosphere and Vacuum Performance Using RF Plasma ing for plasma wall interactions nozzle with multi-axis thrust system verification campaign

16.15 Density Based on Graphene-Ox- Environment Cathode with Pulsating Boost W. Villafana measurement system F. Stesina ide-Semiconductor Structure Y. Guo Chopper Circuit M. Edamoto R. Furuya K. Nagamine

A214   A622   A771  A478  A815  Radio Frequency Microdischarge One to One Comparison of Effects of Pulsating Boost The Sputtering Mechanism of Enabling High-Energy Missions Neutralizer Chemically Energetic and Inert Chopper Power Supply on the Keeper Electrode in Hall Thruster with Nanosatellites by Using F. Filleul Electrospray Propellants Performance of TAL-type Hall J. Chen Ablative Pulsed Plasma Thrusters 16.30 C. Lyne Thruster P. Gessini K. Hasegawa

A788   A563  A534  A920  High-Speed Transient Character- Impact on Performance and Numerical Prediction of Wall The operation of a low-power ization of the Busek BET-300-P Erosion in Hall Thruster using Erosion Morphology on Hall cylindrical Hall thruster with zinc

16.45 Electrospray Thruster Argon and Xenon propellant Thrusters as the propellant D. Courtney J. Yamasaki N. Wu C. Ryan

A746  On the Performance of Arcjet Thrusters using Numerical Mode- ling: A case study of Hydrogen as 17.00 a propellant D. Akhare

Session End → Gala Dinner beginning 18.30 THURSDAY

Areas

Material Technology Commercial Hall Thrusters 1 Hall Thrusters 2 Ion Thrusters MPD Thrusters Innovative / Advanced Thruster Cathodes, Gimbals Propulsion Needs Propulsion Concepts Concepts

HS6 SR4 SR6 SR7 HS5 SR8 HS3 HS2

A249   A600  A115  A487  A127  A493  A164  A188  Comparison of transient behavior Electric Propulsion Develop- Use of Real-Time Spectrum Oscillation analysis in Hall Electric Propulsion Direct-Current Magnetic Field and Current Evaluation of anomalous resistiv- Comparison of waveguide-cou- in a 20 A hollow cathode in a 9 ments at Rafael in 2019 Analysis for EMI Characterization thrusters with 2D (axial-azimuth- Current Transformer (EPDCCT): Density Probe for Steady State ity in a low power magnetic pled and coaxial-coupled ECR kW Hall thruster and a stand- D. Lev of the SAFRAN PPS5000 Hall al) Particle-In-Cell simulations Design and Experimental AF-MPD Thrusters nozzle magnetic-nozzle thruster using a 09:00 alone configuration Thruster T. Charoy Validation A. Behnke S. Hepner thrust balance M. Georgin W. Tighe C. Volkmar S. Peterschmitt

A359   A592  A793  A501  A287  A551  A199  A219  Pulsed Electron Beam Extraction The Ariane Group Electric Life Estimation of Hall Thrusters Enhancing Hall Effect Thruster Non-intrusive measurements of Simultaneous Measurement of Experimental Validation and Optimization of a Low Power ECR from a Hollow Cathode Propulsion Program 2019-2020 using Multi Spectral Imaging Simulations with Deep Recurrent microwave ion thruster by two Cathode Surface Temperature Performance Measurements of Thruster Using Pulsed Power and B. Karadag H. Leiter H. Gole Networks photon absorption LIF and laser Distribution and Plasma Spatial an ECR Thruster Operating on Frequency Mixing Techniques

09.15 P. Shaw Thomson scattering Distribution in Self-Field MPD Multiple Propellants B. Wachs R. Tsukizaki Thruster R. Moloney S. Tauchi

A430   A926  A408  A732  A337  A918  A261  A267  Mechanism Analysis of Cathode Overview of Busek EP Thrusters Terahertz Time-Domain Data-Driven Modeling for Estimation of Erosion Rate for Thrust Performance and Cathode The SpaceDrive Project – Development of the hall effect Low Frequency Oscillation V. Hruby Spectroscopy as an Electric Nonlinear Dynamics of Phys- Surface Material on HAYABUSA2 Temperature Evaluation of EMDrive Thrust Measurements hollow cathode thruster Z. Ning Propulsion Plasma Diagnostic ical Phenomena in Hall Effect by Measurement of Backflow Ions MW Class Quasi-Steady MPD and Analysis L. Chenguang 09.30 N. Brown Thrusters from 10-cm-class Ion Thruster Thruster M. Tajmar C. Greve T. Muranaka S. Tonooka

A603   A861  A792  A348  A310  A262  A363  Replacing keeper orifice plate Application of Helium Line Data-Driven Modeling for A novel optical line-ratio method The Experimental Performances The SpaceDrive Project – Over- Diagnostics and testing with emissive material: emission Intensity Ratio Spectroscopy Nonlinear Dynamics of Phys- for measuring the electron of the 100kW MPD Thruster with view of Revolutionary Propulsion facilities for ionic liquid electro- mechanisms and impacts on to Xenon plasma in Penning ical Phenomena in Hall Effect parameters in the discharge Applied Magnetic Field Efforts at TU Dresden spray thrusters at the Air Force 09.45 hollow cathode discharge discharge Thrusters chamber of xenon ion thrusters Y. Cong M. Tajmar Research Laboratory T. Meng H. Sekine D. Bilyeu X. Zhu D. Eckhardt

A604   A516  A579  A396  A314  A271  A417  Applicability of electride Hall Thruster Plume Measure- Analysis of the plasma discharge Optical plasma diagnostics for Cathode Ablation Performance of Plasma Jet Pack (PJP) REGULUS: Iodine Fed Plasma materials for hollow cathodes ments of Time Resolved Ion in a Hall thruster via a hybrid 2D radio-frequency ion thrusters Applied-Field Magnetoplasma- Technology Propulsion System for Small

10.00 M. Reitemeyer Energy code B. Nauschütt dynamic A. Blanchet Satellites T. Kerber P. Fajardo G. Wang D. Pavarin

A649   A308  A613  A503  A401  A279  A498  Ampere-Level C12A7 Cathode Electron cross-field transport Boundary conditions for a Two-Photon Laser-Induced Anode Power Deposition in Thruster Performance Results for XMET: Design and early testing of Operation with Initial Testing of mechanism observed under the two-dimensional direct kinetic Fluorescence Diagnostics of a an AF-MPDT with Two Unique the 200 kW Peristaltically Driven a xenon microwave electrother- Heaterless Ignition azimuthally inhomogeneous simulation of a Hall thruster Radiofrequency Ion Thruster: Magnetic Field Plasma Accelerator mal thruster

10.15 M. Mcdonald neutral supply in a Hall thruster A. Raisanen Measurements in Xenon and P. Wu J. Slough D. Staab Thursday J. Bak Krypton C. Eichhorn

A690   A449  A619  A525  A544  A290  A638  Hollow Cathode Technology for On-board Plasma Plume Operation of a Low Power Development of a Collisional-Ra- Design of Water MPD Thruster Characterisation of a Rotational Direct thrust measurements Low Power Electric Propulsion Diagnostics for ETS-9 All-electric Hall Thruster with a Shielded diative Model for Plasma Thruster A. Kakami Thrust Balance for Propellantless and design upgrade of an ECR Applications Satellite Magnetically Configuration Optical Diagnostics Propulsion Concepts Utilizing thruster operating on water

10.30 W. Ohlinger K. Kinefuchi L. Garrigues M. Celik Magnetic Levitation with propellant Superconductors D. Staab O. Neunzig

A723   A252  A642  A611  A585  A292  A822  Hollow Cathode Operation with Significant ion acceleration of Influence of Magnetic Field Evaluation of Faraday Probes Current Advances in Optimiza- Influence of cathode grid dimen- Status of HEMPT-NG development Time-Varying Currents Xe ions outside the discharge Strength on Narrow Channel Hall towards its Standardisation for tion of Operative Regimes of sion on discharge characteristics programme at Thales Ulm J. Polk channel in cylindrical Hall Thruster Discharge Operating at Electric Propulsion Testing Steady State Applied Field MPD of IEC thruster S. Weis

10.45 thruster plasmas observed by Very Low Power Q. Koch Thrusters Y.-A. Chan laser induced fluorescence I. Kronhaus A. Boxberger G. Doh 34 IEPC19 Programme Thursday 35

Material Technology Commercial Hall Thrusters 1 Hall Thrusters 2 Ion Thrusters MPD Thrusters Innovative / Advanced Thruster Cathodes, Gimbals Propulsion Needs Propulsion Concepts Concepts

HS6 SR4 SR6 SR7 HS5 SR8 HS3 HS2

A776   A246  A720  A618  A588  A333  A875  Characterization of a 100 Hall Thruster Near-Field Plume Numerical studies of the ExB Test Facility for EMC-Character- Experimental study of the High-Specific-Impulse Operation H2020 MINOTOR: Magnetic

A-class LaB6 hollow cathode for Characterization Through Optical electron drift instability in Hall ization of Electric Thrusters in discharge characteristic in in Diverging Magnetic Field Nozzle Electron Cyclotron high-power Hall thrusters Emission Spectroscopy thrusters Operation using an evacuated AF-MPDT ignition Electrostatic Thrusters with Resonance Thruster 11.00 S. Mazouffre M. Nakles F. Taccogna Reverberation Chamber Y. Wang Argon Propellant D. Packan R. Thüringer D. Ichihara

A845   A515  A437  A738  A759  A382  A897  Total Sputter Yield Character- Development and Validation 3D simulation of rotating spoke in Determination of the Beam Characterization and Improve- Metallic Ion Thruster using Mag- HiperLoc-EP: A new approach for ization of Various Spacecraft of a Time-Resolved Ion Energy a wall-less Hall thruster Divergence of a Gridded Ion ment of Thrust Balance for netron E-Beam bombardment SmallSats Electric Propulsion Materials Distribution Diagnostic Thruster Using the AEPD Platform High Power Applied Field MPD

11.15 K. Matyash K.-Y. Chen J. Stark J. A. Young M. Baird C. Bundesmann Thrusters G. Herdrich

A929   A734  A347  A777  A385  A941  Additively Manufactured Hollow HK40 Hall Thruster Plume Plasma Study of the Electron Cyclotron Planar probe array for bidimen- Thrust Generation in Electro- Development of the Xenon Cathode Keepers with Integral Measurements with Retarding Drift Instability inside Hall Effect sional mapping of the ion flux static-Magnetic-Hybrid Plasma Cold Gas Thruster to Support Radiation Shielding Potential Analyzer, Faraday Probe Thrusters with a fluid code profile of a miniaturized ion Thruster All-Electric Propulsion Missions 11.30 M. S. Mcdonald and Langmuir Probe V. Joncquieres thruster A. Sasoh I. Johnson U. Kokal L. Habl

A155   A387  A726  A167  A475  Onset criteria for the plume Study of two different discharge Development of 1D Magneto-stat- Near Field Probe Measurements Design and Performance Test of mode oscillation in hollow modes in Hall thruster ic Two-Fluid Plasma Simulation of in the Plume of a NEXT Ion a RF Plasma Bridge Neutralizer

11.45 cathodes I. Khmelevskoi a Hall Effect Thruster Thruster D. Spemann M. Georgin R. Sahu N. Arthur

A667   The neutral gas properties in orifice hollow cathode before Lunch Break & Poster Session

12.00 its ignition Y. Jia

Plenary Lecture Audimax BEPI Colombo 14.00

A823  A841  A733  A171  A195  A488  A467   BEPI- Colombo Electric Non-intrusive Characterization Coupling Non-Maxwellian View Measurement of a Concentric A Novel Laser Ablation Magneto- Inductive Plasma Thruster (IPT) Performance Analysis of the

Propulsion in Mercury of the Wear of the HERMeS Factor Model to Octree Based Split-Ring Resonator Microplasma plasmadynamic Thruster for an Atmosphere-Breathing Capacitively Coupled Radio Thursday R. Velasco Valencia Thruster Using Optical Emission Particle VDF Compression for for Miniature Ion Engines Y. Zhang Electric Propulsion System: Frequency Thruster

15.00 Spectroscopy Accelerated Spacecraft-Plume K. Xu design and set in operation A. Quraishi T. Gray Simulation F. Romano R. Martin

A305  A932  A880  A175  A313  A500  A577   BepiColombo - Solar Electric Internal Probe Studies of a Low Particle-In-Cell model of the Design and Experimental Study of Development of High Power Review of Dualmode/Multimode Proposal and Performance Propulsion System Operations Voltage Hall Thruster dynamic of the electrons between an Miniature Ion Thruster Magnetoplasmadynamic Space Propulsion Evaluation of Microwave-Driven for the Transit to Mercury J. L. Ross the two walls of Hall thrusters J. X. Ren Thrusters in BICE and Beihang J. Rovey In-Tube Accelerator Concept

15.15 C. Steiger including realistic secondary University M. Takahashi electron emission data Y. Li M. Villemant

A606  A384  A215  A238  A542  A552  A594   BepiColombo – The Mercury Incoherent Thomson scattering Numerical solutions of Density Preparation of Space Experiment Applied-Field MPD Thruster with Interaction of Ultraviolet Indirect electrothermal Transfer Module investigations of a low-power Gradients Instability in a Hall with Electric Propulsion System High Current Heater-less Hollow Light-emitting Diodes and Solid acceleration of a cold gas jet H. Gray Hall thruster in standard and Thruster Plasmas Based on Radio-Frequency Ion Cathode Polymers for Micropropulsion through interaction of an arcjet

15.30 magnetically-shielded configu- S. Singh Thruster aboard the International J. Yamasaki Applications exhaust flow for space propulsion rations Space Station H. Horisawa applications B. Vincent R. Akhmetzhanov Y. Arai 36 IEPC19 Programme Thursday 37

BepiColomboMaterial Technology Commercial Hall Thrusters 1 Hall Thrusters 2 Ion Thrusters MPD Thrusters Innovative / Advanced Thruster Cathodes, Gimbals Propulsion Needs Propulsion Concepts Concepts

HS6 SR4 SR6 SR7 HS5 SR8 HS3 HS2

A615  A617  A239  A872  A605  A610   BepiColombo – MEPS Characterization and perfor- Atmospheric Ramjet Thrust Unit Development of a 10-30 kW Hybrid Electric Propulsion Informing the design of pure-ion commissioning activities and mance measurements of 40 on the Base of High-frequency Augmented Field MPD Thruster System based on Water electrospray thrusters via T6 ion thruster performance W-class and 100 W-class Hall Ion Thruster at SITAEL Electrolysis simulation of the leaky-dielectric 15.45 during early mission operations thrusters M. Suvorov A. Kitaeva N. Harmansa model with charge evaporation P. Randall T. Hallouin X. Gallud Cidoncha

A824  A528  A349   A240  A450  A621  A643   BepiColombo – Development Efforts on a Laser Microinstabilities and rotating Characteristics of Radio-Fre- Performance of Applied Field Advanced Cusp Field Thruster Physics and performance of the A mission overview Thomson Scattering Diagnostic spokes in the near-anode region quency Ion Thruster with an MPD Thruster with Various with a 3D-printed discharge Alternative Low Power Hybrid N. Wallace for Electric Propulsion Applica- of a Hall thruster Additional Magnetic Field in the Propellants channel - Performance with Ion Engine (ALPHIE) for space 16.00 tions J.-P. Boeuf Ionization Area S. Ide Iodine and Xenon propulsion T. Matlock V. Kozhevnikov M. Vaupel J. González

A494  A598  A582   A339  A669  A645  A775   BepiColombo – MTM and MEPS Experimental Study on the Experimental characterization Ring Cusp Ion Thruster IT-200PM Thrust Evaluation of a Small- 100 kW Nested Hall Thruster Azimuthal Induced Current Integration and Verification Influence of Magnetic Field on and modeling of ID-HALL, a A. Lovtsov seized SF-MPD Thruster High Power System Demonstra- Formation and Ion Acceleration K. Kempkens the Performance of Low-power double-stage Hall thruster with K. Ueno tion in an Inductive Radiofrequency 16.15 Hall Thrusters an inductive ionization stage S. Shark Plasma Thruster X. Yi Á. Martín Ortega H. Sekine

A586  A447   A574  A870  A693  A829   BepiColombo - Solar Electric Performance Evaluation of a Test Campaign on the novel Plasma Plume Characteristics of 100kW Nested Hall Thruster Two-dimensional Full Propulsion System Test and 100-W Class Hall Thruster Variable Isp Radio Frequency Mini Cluster Operation of Self-Field System Development Particle-In-Cell Simulation of Qualification Approach H. Watanabe Ion Engine Magnetoplasmadynamic J. Jackson Magnetic Sails in Formation Flight 16.30 S. Clark M. Smirnova Thruster A. Wada Y. Murayama

A770  A338   A625  A921  A692  A903   BepiColombo Solar Electric Design and experimental Status of HEMPT Electric Traveling Wave Thruster System 13kW Advanced Electric Propul- An experimental revisit of plasma Propulsion Plasma-Spacecraft research of a micro-newton Propulsion Flight Hardware for Development sion Flight System Development phenomena on Helicon Plasma Interactions: Comparison of cusped field thruster Heinrich Hertz Satellite D. Cope and Qualification Thrusters

16.45 Flight Data with Numerical M. Zeng A. Lazurenko J. Jackson J. Navarro Cavalle Modelling F. Filleul

A741  A816   A797  A329  A712  A931   Erosion and Lifetime of the Scaling of spoke rotation fre- Exprimental studies on the effect Research on the 500kW The SpaceDrive Project – Development of Dielectrophoretic Aurora Low-Power Hall Effect quency within an ExB Discharge of the magnetic field and the Class Superconducting Progress in the Investigation Force Feeding Subsystem for Thruster A. Powis electrical potential inside the Strong Magnetic Field High of the Mach-Effect-Thruster Liquid Pulsed Plasma Thruster Thursday 17.00 J. Makela water ion thruster Power Magnetoplasmadynamic Experiment C. Dobranszki Y. Ataka Thruster Technology M. Monette C. Zhou

A298  A352   A806  A801  A774  A365   Pole Erosion Measurements for Neutral gas instabilities in Hall A Nouvelle Neutralization Business Cases and System Development of a deployable RF Power - Plasma Coupling the Development Model of the thrusters, Part I: Measurements Concept for RIT-µX Miniaturized Architecture for Superconduc- vacuum arc thruster system for Experimental Results in a Helicon Magnetically Shielded Miniature Radio Frequency Ion Thruster tor-based Applied Field Magneto the post-mission disposal of Plasma Thruster Prototype

17.15 E. Dale Hall Thruster (MaSMi-DM) Systems Plasma Dynamic Thrusters micro/nano satellites V. Gómez R. Lobbia H. Leiter M. La Rosa Betancourt M. Kim

A209  A432   A808  A886  A940   Hall Thruster Erosion Meas- Driving Low Frequency Oscilla- The RIT 2X High Performance Ion Development Roadmap of A thruster using magnetic urement by Time-Resolved tions in Hall Thruster Thruster System Qualification SITAEL’s RAM-EP System reconnection to create a high-

17.30 Cavity-Ring Down Spectroscopy Y. Raitses Program T. Andreussi speed plasma jet Y. Egawa J.-P. Porst S. Bathgate

A332  A889   A842  Numerical simulation and Gradient-drift instability as an Charge State Thrust Correction experimental research on low origin of spokes in Hall thrusters Factor for NEXT: DART Mission

17.45 power Hall thruster with long life N. Marusov M. Crofton Y. Ding 38 IEPC19 Programme Thursday 39

Material Technology Commercial Hall Thrusters 1 Hall Thrusters 2 Ion Thrusters MPD Thrusters Innovative / Advanced Thruster Cathodes, Gimbals Propulsion Needs Propulsion Concepts Concepts

HS6 SR4 SR6 SR7 HS5 SR8 HS3 HS2

A341  A354   A844  A293  A 2000 Hours Life Test of a 5 Neutral gas instabilities in Hall Deposition Rate Measurements in Back-vacuum Retarding Poten- kW Multi-mode High Specific thrusters, Part II: Theory NEXT Ion Engine Plume for DART tial Analyzer for Investigation of Impulse Hall Thruster HEP- E. Dale Mission IEC plasma properties 18.00 140MF J. Young Y.-A. Chan W. Mao

A749  A632   A853  A434  Prediction of liner erosion and Influence of double-stage NEXT Single String Integration Beam Plasma Expansion of a life estimation of Stationary operation on breathing oscilla- Tests In Support of the Double Helicon Plasma Source Plasma Thrusters using Machine tions and rotating spokes in the Asteroid Redirection Test Mission Z. Zhang 18.15 Learning ID-HALL thruster R. Thomas S. Bhat A. Guglielmi

A433   A859  A448  Use of electrostatic probes for Experimental Characterization of Modeling and Optical Diagnos- characterization of the electron the Microwave-Discharge Water tics of Iodine Fed Helicon Type cross-field current in ExB plasmas Ion Thruster for CubeSats Thrusters by a Detailed Global 18.30 Y. Raitses Y. Nakagawa Model (DGM) K. Katsonis

A323   A928  A682  Experimental study on the effect Arclight: a plug-in gridded ion A Detailed Global Model for of propellant asymmetrical propulsion system for small Modeling and Optical Diagnos- distribution on plasma potential satellites tics of Low Power Propulsion

18.45 distribution in a Hall effect P. Bauer Devices Fed by CO2 thruster C. Berenguer M. Ding

Session End 19.00 Thursday FRIDAY

Areas

Hall Thrusters Ion Thrusters Propellant Storage Mission Diagnostic Hall Thrusters Mission

/ Feed Systems ←

SR7 HS5 SR5 HS2 SR6 SR7 HS2

A665   A145  A601  A192  A773  A543   A411  Plasma fluctuations Radio-frequency biasing Innovative Xenon/Krypton Development of the ESA Propulsion Laboratory Towards Predictive Kinetic Simulations of Electric Propulsion Characterisation for a measurements in a Hall of ion thruster grids FMS (Feed Management Psyche Mission for NASA's E. Bosch Borràs Plasma Thrusters Stand-Alone Mars CubeSat

Thruster T. Lafleur System) for Electric Discovery Program 10.45 I. Kaganovich K. V. Mani 09:00 N. Yamamoto Propulsion D. Oh P. Barbier A545   A727  A687   A431  A871  A244  A374  Fluid modeling of gradient-drift turbulence and Microsatellite Electric Propulsion System Axial-azimuthal high-fre- M S of the Erosion and Simulation And Exper- Electric Propulsion for the Three-dimensional transport in ExB plasmas (MEPS) Project Status in 2019

quency instability modes Contamination Effects on imental Study on Xeon Psyche Mission Vector Measurement of EP 11.00 A. Smolyakov D. Lev in a Hall thruster fluid the CAESAR Spacecraft Mass Flow Regulating S. Snyder Propellant Flow within a model L. Bermudez Characteristics of the Vacuum Chamber E. Bello-Benítez Proportional Valve Based Y. Nakayama

09.15 A691   on Unimorph Ring- New insights into electron transport due to Shaped Piezoelectric azimuthal drift in a Hall effect thruster Actuator 11.15 K. Hara X. Wang

A454   A507  A400  A654  A517  A569   Effect of magnetic A global performance Development of Sitael HT100 Missions: In-situ microscopy of field configuration on model of Gridded Ion Porous-Metal-Restrictor uHETSAt and PLATiNO ion-induced erosion of Assessment of the thermodynamic and fluid approximations for electrons in plasma thruster discharge characteristics Thrusters Based Xenon Flow Control T. Misuri plasma-facing surfaces

11.30 plumes 09.30 in permanent magnet E. Ahedo Galilea Modules A. Ottaviano thrusters with cusped field G. Hang Y. Hu S. Liang A304   A472   A908  A442  A138  A258  Characteristic Transient Phenomena of Hall SPT Phenomenology Performance Assessment Integration and Function- Status Update on the Thrust measurements Effect Thrusters

V. Kulygin of a Micro- Gridded Ion al Test Results of Xenon Electric Propulsion using plasma pressure 11.45 A. Komarov Thruster Design Feed Unit for Electric Subsystem of TURKSAT6A measurements in the 09.45 P. Harte Propulsion Subsystem Communication Satellite plume: a feasibility study Y. Yurttas B. C. Aydin P.-Q. Elias A758   Plasma instabilities in cross-field configuration: A479   A541  A923  A887  an analysis of the relevance of different modes

Predicting secondary A Novel Miniature Xenon Final Operations of the Recent Advances in 12.00 for electron transport electron emission rate in Feeding Module for Hall Dawn Ion Propulsion Plasma Diagnostics at IRS S. Tsikata Hall Effect Thrusters Electric Thruster System andthe Success- G. Herdrich

10.00 A. Tavant C. Guan ful Conclusion of the A843   Dawn Mission Experimental Correlation between Anomalous C. E. Garner Electron Collision Frequency and Plasma

12.15 Turbulence in a Hall Effect Thruster A514   A891  A429  A345  Z. Brown Enhancing thrust by Towards a Microfluidic The Comet Astrobiology Development of a Flight ion-neutral collisions and Flow Control Unit for Exploration Sample Electric Propulsion A718   by oscillating EM fields HEMP Thrusters Return (CAESAR) Mission Diagnostic Package Investigation of cross-field electron transport 10.15 (EPDP) for EP Satellite A. Fruchtman J. Haderspeck M. Sekerak in a 100-W class Hall Thruster using a full Platforms

12.30 particle-in-cell simulation T. Trottenberg S. Cho A523   A917  A927 

A593   Friday Effects of large scale Qualification Program of a Mars Sample Return structures on anomalous Composite Overwrapped - Earth Return Orbiter: Simulation of radial electron dynamics in a Hall transport in PIC simula- Xenon Propellant Tank for ESAs next Interplanetary effect thruster

tions of Electron Cyclotron a GEO Satellite Mission Electric Propulsion 12.45 A. Domínguez-Vazquez 10.30 Drift Instability in Hall S. Ontaç Mission Concept thrusters O. Sutherland A. Smolyakov Technical Visits ← 13.00