IEPC Programm Master 2 · mover permanent magnets for changing a magnetic field Y. Takao A835 Computer Modeling of Non-Emission Electron Source with High Frequency Ionization S. Roshanpour

Programme

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Overview 04

Monday 10

Tuesday 20

Wednesday 24

Thursday 34

Friday 42

Contact

Dr. Alexander ReissnerGeneral ChairENPULSION→ [email protected]

Dr. Carsten ScharlemannChair of Technical CommitteeFachhochschule Wiener Neustadt GmbH→ [email protected]

Katrin FanglChair of Organizing CommitteeFOTEC Forschungs- und Technologietransfer GmbH→ [email protected]

4 5IEPC19 Programme

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Monday 16 Tuesday 17 Wednesday 18 Thursday 19 Friday 20

09:0

0 Plenary Lecture Welcome Speech / David C. Byers Memorial Panel

Paralell Sessions Paralell Sessions Paralell Sessions Paralell Sessions

10.0

0 Plenary LectureAgencies

11.0

0 Plenary LectureIndustry

Conference TourMelk Abbey

12.0

0 Lunch / PostersessionArkadenhof

LunchArkadenhof

Lunch / PostersessionArkadenhof

13.0

0 Technical VisitsVineyard Visit

13.3

0

Plenary LectureLEO

14.0

0

Paralell Sessions

Plenary LectureEuropean National Agencies

Plenary LectureBepiColombo

15.0

0 Paralell Sessions Paralell Sessions Paralell Sessions

16.0

017

.00

18.0

0 Gala DinnerRathaus

19.0

020

.00

21.0

0

ERPS MeetingLocation

Shedule / Floorplan

Seminraraum 8 Seminraraum 7 Hörsaal 6 Hörsaal 5

Hörsaal 2Hörsaal 3

Seminraraum 6Seminraraum 5

Seminraraum 4

Raised Ground FloorExhibition

Lower Level Sessions

Audimax

6 7IEPC19 Programme

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A109 Heat Trnsfer Simulation in Radio-Frequency Ion ThrusterV. Abgaryan

A117 Non-preheated Hollow Cathode for Hall ThrustersO. Petrenko

A125 Analysis and test on magnetic field for hall thruster based on perma-nent magneticJ. Hu

A130 Performance Charac-teristics of High-Power Steady-State MPD Thrusters with Divergent and Cusp Magnetic Fields Using Permanent Magnets for In-Space PropulsionH. Tahara

A131 Performance Character-istics and Interior Plasma Phenomena of High-Power and High-Specific-Impulse Hall Thrusters for In-Space PropulsionH. Tahara

A132 Study on Low-Power Water-Cooled and Anode-Radiation-Cooled DC Arcjet Thrusters Using HAN and Water Propellants with Special Vaporing SystemsH. Tahara

A133 Development of Commercially-Available Electrothermal Pulsed Plasma Thruster Systems for Powered Flight of Micro/Nano-Satellites at Osaka Institute of TechnologyH. Tahara

A134 Development of the Osaka Institute of Technology 2nd PROITERES Nano-Satellite with High-Power Electro-thermal Pulsed Plasma Thrusters for Powered FlightH. Tahara

A135 Research of Debris Removal Systems by Electric Propulsion and Development of the 4th PROITERES Nano-Satellite for Its Practical Space Experiments at Osaka Institute of TechnologyH. Tahara

A162 Studies on Helicon Plasma Thruster and Measurement MethodsD. Kuwahara

A186 Design of Modular, High Efficient Anode Power Supply for Low Power Hall ThrustersS. Deshpande

A194 A Thrust Balance for the MINOTOR ECR ThrusterS. Scharmann

A201 Design and Construction of a Rotating Magnetic Field, Field-Reversed Configura-tion (RMF-FRC) ThrusterC. Sercel

A231 Longterm testing and evaluation of the vacuum arc thruster system using multi-element cathodesM. Kuehn

A250 A 3D Hybrid-IFE-PIC-MCC model for the discharge chamber simulation of ion thrustersY. Cao

A256 2D Particle-in-Cell Simulation of Current Characteristics in Three-Grid Ion OpticsA. Sun

A269 Evaluation of Coaxial Short-pulse Laser-assisted Pulsed Plasma ThrustersK. Sato

A286 Investigation of Antenna Current and Regime Transition in Electrodeless Inductive Plasma Gener-atorsR. Georg

A316 Experimental study on 25w pulsed plasma thruster electric propulsion systemX. Chen

A334 Low frequency ionization oscillation model with azimuthal dimension in a Hall thrusterJ. Bak

A335 Feasibility study of sublimable substance as an alternative propellant to xenon in ion thrustersM. Adachi

A350 Overview of SITAEL Electric Propulsion DevelopmentsT. Misuri

A399 Frequency-time structure and mathematical models of SPT emission in the radio-frequency rangeA. Plokhikh

A414 Numerical Investigation of Ignition in a Novel Positron-Catalyzed Fusion Propulsion ConceptL. Brieda

A416 1-D PIC Model of a Magnetically Enhanced Plasma ThrusterM. Minute

A436 Dynamic Acceleration Region Sizing and the Impact on Breathing Mode OscillationsJ. Little

A438 Study of two-stage pulsed plasma thruster with special propellant combined ion liquid and resin manufac-tured by 3D printerJ. Saiki

A440High Power Laser Powered PropulsionK. Mori

A483 Numerical Simulations of a Capacitively Coupled RF Micro-ThrusterA. Popoli

A486 Characteristics of laser sustained plasma using argon and methane for on board laser-based thrusterM. Matsui

Poster SessionMonday 16Thursday 19

A489The Effect of Plasma Ion Current on the Acceleration of Field Reversed Configu-ration PlasmoidX. Sun

A490A PIC/MCC simulation on the initial ignition stage of a 20mN Hall thrusterJ. Yizhou

A509Experimental study of plasma parameters and quantitative analysis of discharge instabilities in 500W Hall effect thrusterV. Desangles

A568Metallic Vapor Thruster using Field-emitted Electron BombardmentsP.-Y. Chang

A570Development of a 200 W Class Hall Thruster for an Active Debris Removal SystemN. Yamamoto

A587Fluid simulation of low frequency oscillations in Hall thrustersA. Rostek

A636Study on the Influences of Magnetic Field Configura-tion on TAL Hall Thruster Discharge Chamber Plasma CharacteristicsC. Liu

A641Design and test of 1cm-class RF Ion Micro Propulsion System for Taiji Program in SpaceJ. He

A6742D (axial-azimuthal) Particle-In-Cell benchmark for ExB dischargesT. Charoy

A697Experiment Study on the Property of 10cm ECR Ion Source Operating on Different Wave Radiation ModeZ. Hu

A707Full-particle PIC/MCC numerical simulation of 2 cm ECRIT ion sourceX. Xia

A716Study of the electron anomalous transport in a Hall effect thruster using a 2D multi-fluid simulationC. Gonzalez

A763Particle-in-cell numerical simulations of an helicon double-layer thrusterR. Miranda

A764Analysis of Erosion of Plas-ma Thrusters for Brazilian Space Missions Through Numerical SimulationsL. Braga

A799Thermal analysis of diode-laser coupled fiber-tip heat source for high-temperature generationT. Matsuo

A800Current Tests of the Miniature Gallium Field Emission Electric Propulsion ThrusterM. Xu

A803Probe study on ion beam and backflow for different electric propulsion technologiesV. Hugonnaud

A807Combined optical emission and laser absorption spectroscopy of Xenon gridded ion thrusterR. Kozakov

A809Experimental Evaluation of the Micro Water Thruster Recovering Waste Heat of a SpacecraftK. Nishii

A812Development of Microwave Discharge Ion Engine with Variable Magnetic Field by Mover Permanent Magnets to Axial and Radial DirectionsY. Takao

A813Integrated simulation solutions for the plasma and transversal physics in electric propulsion systemsM. Kubecka

A814Line-Integrated Barium Laser Absorption Spectros-copy Along Cathode AxisN. Wirgau

A821Development of microwave discharge ion engine with mover permanent magnets for changing a magnetic fieldY. Takao

A835Computer Modeling of Non-Emission Electron Source with High Frequency IonizationS. Roshanpour

A857Molecular Dynamics Simulations of Nanodroplet Break-up for Ionic Liquid Electrospray ThrustersY. Takao

A866Basic Characteristics of Plasma Thruster using ICR Heating in Sheet PlasmaA. Tonegawa

A869A Cylindrical Hall Thruster for Mars Air PropulsionY. Nakayama

A919Investigation of Electron Yield in a Ferrite Core RF Cathode to be Used in Plasma ThrustersM. Celik

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 11IEPC19 Programme

Mon

day

Material Technology Cathodes, Gimbals

Field Emission /Colloid Thrusters

Hall Thrusters 1 Hall Thrusters 2 Ion Thrusters Pulsed Plasma Thrusters

Commercial Propulsion Needs

Global Strategic Invests

Innovative Concepts

HS6 SR5 SR6 SR7 HS5 SR4 HS2 SR8 HS3

09.0

0 Wecome Speech Audimax

09.3

0 David C. Byers Memorial Panel Audimax

10.0

0 Plenary Lecture AudimaxAgencies

11.0

0 Plenary Lecture AudimaxIndustry

12.0

0

Lunch Break & Poster Session

14.0

0 Plenary Lecture AudimaxEuropean National Agencies

14.0

0

A299 The Effect of Neutral Gas Injection in the Keeper Orifice of a 25-A class Hollow CathodeS. Hall

A149 Development of Ionic Liquid Electrospray Thrusters with a Massive Emitter Array for Higher Thrust DensityY. Takao

A129 Hybrid Data-Driven and Physics-Based Model for Plasma Turbulence in a Hall Effect ThrusterB. Jorns

A532 Spatiotemporally Resolved Ion Velocity Distribution Measure-ments in the 12.5 kW HERMeS Hall ThrusterV. Chaplin

A154 Three-Dimensional Parti-cle Simulations of Electron Extraction for a Miniature Microwave Discharge Neutralizer Using Water as the PropellantY. Sato

A184 The Modular Micro-Cathode Arc ThrusterS. Hurley

A303 Versatile Xenon Flow Controller for Extended Hall Effect Thruster Power RangeG. Lenguito

A189 Activities of the H2020 Strategic Research Cluster on Space Electric Propulsion (2015-2019)J. Lopez Reig

A202 Performance Scaling of Drag-Modulated Plasma AerocaptureC. Kelly

14.1

5

A300 The Role of Neutral Pressure Due to Anode Ge-ometry in Hollow Cathode Mode TransitionsS. Hall

A173 Laboratory Demonstration of a Staging System for Electrospray ThrustersO. Jia-Richards

A147 Modular Comprehensive Modeling of Plasma Behavior in Hall ThrustersT. Andreussi

A531 Ion Velocity Measure-ments in the Magnetically Shielded Miniature Hall Thruster (MaSMi) Using Laser-Induced Fluores-cenceV. Chaplin

A309 Lifetime Evaluation of Microwave Discharge Neutralizer using Numerical AnalysisN. Hiorike

A185 A Performance Comparison of solid Propellants in a Surface Arc Thruster: Sulfur and TeflonS. Shimhanda

A505 New Propellant Approval at Apollo Fusion Inc.—Activities to Support Industry and Regulatory Approval of New PropellantM. Haverty

A602 Evolution and Characteristics of the Use of Electric Propulsion for Low Earth Orbit SatellitesD. Lev

A254 Fluid-kinetic propulsive magnetic nozzle model in the fully-magnet-ized limitM. Merino

14.3

0

A406 Development of a Diamond-Based Cold Cathode for Space Propulsion ApplicationsI. M. Ahmed Rudwan

A225 Colloid Micro-Thruster (CMT) Component Development Testing Towards Meeting LISA Mission RequirementsN. Demmons

A204 Model for the Increase in Thruster Efficiency from Cross-Channel Coupling in Nested Hall ThrustersL. Su

A513 Charge Exchange Collision in the Plume of a 200 W Laboratory Hall ThrusterM. Baird

A218 Numerical study of microwave discharge ion thruster µ10Y. Yamashita

A273 A Coupled-inductive Energy Storage Power Processing Unit for Micro-cathode Arc ThrusterJ. Long

A721 Development of an additively manufactured mass, volume and cost optimised fuel tank for microsatellite propulsion systems MiniTankA. Bell

A711 The Importance of Electric Propulsion to Future Exploration of the Solar SystemJ. Cassady

A420 Theoretical scaling laws for water-vapor propellant thrustersA. Sheppard

Monday


Mon

day

Monday






Innovative Concepts


14.4

5

A557 Development of a Microwave Discharge Cathode for a 200 W Class Hall ThrusterT. Morishita

A372 Pure Ionic Electrospray Extractor Design Optimization Utilizing Additive ManufacturingR. Antypas

A220 Study on the Influence of Electron Conduction Paths on the Ignition Process of Hall ThrusterW. Li

A868 Performance Improvement and Testing of a Micro-wave ECR Neutraliser for a Gridded Ion ThrusterU. Khan

A556 Performance Evaluation and Development of Air Bearing Thrust Measurement System of Surface Arc ThrusterK. Hiraka

A456 Progress in Automated System Design by Evolutionary Algo-rithmsM. Ehresmann

A753 Application of Solar Electric Propulsion in the Emerging Satellite Servicing IndustryM. Glogowski

A439 Numerical study on a conical shaped target for Laser Fusion RocketT. Yamamura

15.0

0

A629 Development of a C12A7 Electride Hollow Cathode and Joint Operation with Plasma ThrustersC. Drobny

A277 The Effect of Ionic Liquid Composition on Ion Electrospray Thruster PerformanceC. Miller

A459 Magnetic Circuit Optimization for Hall Thrusters DesignT. Andreussi

A276 Experimental Investiga-tion of the Implications of Nesting Multiple Hall Thruster ChannelsS. Cusson

A706 Two-Dimensional Particle-in-cell Simulation of 10 cm Microwave NeutralizerY. Fu

A616 Development of Pulsed Plasma Thruster for a Pico-SatelliteM. Sammut

A826 HEMPT-Strategy to address current and future Space MarketE. Bosch

A778 Spacecraft perspective trends and their propulsion systemsA. Sizovi

A553 Local Plasma Flow Coupling with Plasma-wave Interaction in Helicon Plasma ThrustersB. Tian

15.1

5

A644 Comparison of the thermi-onic emission properties of LaB6 and C12A7N. G. Kottke

A284 Micro-Newton Electros-pray Thrusters for China’s Space-Borne Gravitational Wave Detection Mission (Tian Qin)P. Song

A470 Theoretical Models of Suppression of Instabil-ities in Hall Thruster by Shear of Magnetic FieldA. Kapulkin

A288 EP system development and functional validation tests for the Electra GEO satelliteV. Garcia

A272 Hybrid-PIC Simulation of Back-sputtered Carbon Transport in electric propulsion test facilityH. Zheng

A899 Filament-fed Pulsed Plasma Thruster (FPPT) for Small SatellitesD. Carroll

A212 The Benefits of Continued Advances in the Propulsive Capability of the Electric GEO Communications SatelliteJ. Trescott

A780 Compatibility of electric propulsion and spacecraft: general requirementsE. Tverdohlebova

A717 Validation of an Equivalent Circuit Model for Rotating Magnetic Field Field-Reversed Configuration ThrustersJ. Woods

15.3

0

A482 Development of High Current LaB6 hollow CathodeW. Yang

A344 Characterisation of electrospray microemit-ters fabricated by planar and 3D photolithographyT. Henning

A278 A Comparison of Possible Mechanisms for Facility Effects on Hall Thruster OperationT. Matlock

A142 Hall thrusters develop-ment at Exotrail: pres-entation and experimental investigationA. Gurciullo

A302 EMC considerations for RIT engines based on 3D full-wave field simulation of electromagnetic emission of their RF coilsT. Sommavilla

A657 A Vacuum Arc Ion Thruster for SmallSat ApplicationsJ. Kolbeck

A210 EP orbit raising: environmental effects impact on satellites, modelling and challengesB. Zitouni

A876 Propulsion subsystem for a stand alone interplanetary CubeSatD. Feili

15.4

5

A695 Featherweight Heaterless Hollow Cathode Charac-terizationM. Mooney

A650 A Novel Variable Mode Emitter for Electrospray ThrustersP. Wright

A306 A comprehensive xenon collisional-radiative model of atomic and ionic excited levels for Hall thrusterY.-F. Wang

A114 Hall Thruster ST-25 designed by Space Electric Thruster Systems (SETS)O. Petrenko

A496 Numerical simulation of plasma discharge in RF ion thrusterR. Rakhimov

A860 Optical measurements of ablation process of double-cylindrical pulsed plasma thrusterT. Inaba

A883 More added value? – an investi-gation on the commercial benefit of different EP technologies for orbital propulsion instancing H2020´s GIESEPPC. Dietz

A275 High power electric propulsion: MARS plus EUROPA - already beyond 2025!F. Jansen

16.0

0

A768 Evaluation of Iodine Compatible Hollow Cathode ConfigurationsS. Thompson

A223 Direct Thrust Meas-urement and Plume Characterization of a Porous Electrospray ThrusterC. Ma

A762 Stationary Profiles and Axial Mode Oscillations in Hall ThrusterA. Smolyakov

A791 Performance Comparison of a 2 kW Hall Thruster with Heaterless Cathodes Mounted on the Outer Pole Piece and on the Thruster CenterlineT. Andreano

A905 Analytical and numerical simulation of Ring Cusp Discharge ChamberF. Cannat

A421 Performance and Efficiency of Electric Solid Propellant in a Pulsed Plasma ThrusterM. Glascock

A790 Development of a 100 mN Horizontal Torsion BalanceB. Seifert

A607 VENUS - Updates on Technologi-cal Mission Using IHETD. Lev

A176 🌴 Effects of magnetic shielding on the performance of Multi-cusped field thrusterP. Hu

16.1

5

A802 Diagnostic analysis of a 30 A heaterless hollow cathodeA. Daykin-Iliopoulos

A296 Experimental Validation of a Dielectric Electrospray Emitter with a Directly Deposited Thin Film ElectrodeA. Kimber

A846 Proportional Thermal Model for Hall Thrusters with Magnetic ShieldingM. Porto

A441 Development Status of 6-kW-class Hall Thrusters at JAXAI. Funaki

A367 Plasma characteristics in the backflow region of ion thruster plumes using kinetic and electron fluid modelsN. Nuwal

A659 Micro-cathode arc thruster improvement by the second MPD stageK. Daniels

A413 Design and testing of a μN - mN torsional thrust balance with wireless microwave power transmissionK. Swar

A418 Electric Propulsion for Small Satellites: A Case StudyP. Lascombes

A243 🌴 Electric Propulsion Pointing Mechanism EPPM for the Spacebus Neo PlatformA. Derntl


Mon

day

Monday






Innovative Concepts


16.3

0

A890 Characterization of a Fixed-Volume Release System for Initiating an Arc Discharge in a Heaterless Hollow CathodeR. Ham

A471 Development and Characterization of an Ionic Liquid Electrospray Thruster with a Porous Metal Blade ArrayX. Liu

A264 A thermo-mechanical analysis with the use of tasks in a non-linear for-mulation for a low-thrust thruster calculations during lifetime prediction with the SPT-50 thruster as an exampleO. Olshanskaya

A342 Parametric study of 1,5- and 2.5-kW Hall Thrusters with an external discharge zoneA. Lovtsov

A529 Study of Ion Thruster Backflow Characteristcs with Neutralization Using Kinetic PIC-DSMCD. Levinl

A662 Experimental Analysis of Cusped Magnetic Field Focusing on Vacuum Arc ThrustersM. Laterza

A784 TIDBIT - Thruster In-Space Diagnostics with Bus Integrated TelemetryT. Matlock

A373 🌴 Plasma Magneto-Shell Aerocap-ture for Manned Mars Missions and Planetary Deep Space OrbitersJ. Slough

16.4

5

A422 The development of the Integrated Thruster Unit ITU100 and ITU140A. Zarakovskiy

A522 Performance of a Fully Conventionally Machined Liquid-Ion Electrospray Thruster Operated in PIRM. Natisin

A392 Laboratory tests of 10.5kW Hall thruster with external layerA. Shashkov

A473 Parallel codes using non-uniform meshes and view factor model methods for particle in cell-Monte Carlo collision (PIC-MCC) simulation in ion thrusterR. Pan

A798 An investigation of alternative propellants for pulsed plasma thrustersW. Y. L. Ling

A211 Thrusters modelling, propellant choice and plume expansion: openPlumeEP capabilitiesB. Zitouni

A398 🌴 Modeling, Simulation and Testing of a Magnetically Enhanced RF Plasma Source for a High Power Electromagnetic ThrusterX. Wen

17.0

0

A881 Harmonization of European Mechanisms for Electric PropulsionM. Toso

A787 Reconstructing Elec-trospray Plume Current Spatial Distributions using Computed TomographyD. Courtney

A681 Status of Research Activities on Electric Propulsion at CIRAV. Salvatore

A740 Performance of the Aurora Low-Power Hall Effect ThrusterJ. Sommerville

A565 Numerical simulation of electrospray thruster extraction for highly conductive propellantsH. Huh

A554 Ignition Capability of Pulsed Plasma Thruster with Green Liquid PropellantJ. Aoyagi

A123 Cryopumping Challenges of EP-Propellants in DLR’s Electric Propulsion Test FacilityA. Neumanni

A547 🌴 Electric Propulsion Activities at the UCLA Plasma Space Propulsion LaboratoryR. Wirz

17.1

5

A289 Development and Qualification of an Electric Propulsion Thruster Orientation Mechanism for the Electra GEO satelliteV. Garcia

A794 Investigation of Electros-pray Plume Composition during Voltage TransientsE. Petro

A241 PPS®X00 Hall Thruster Development Status at SafranJ. Vaudolon

A910 Performance, Stability, and Wear Characteriza-tion of a Sub-Kilowatt Hall ThrusterH. Kamhawi

A612 Elegant Approach for solving the Conservation Laws in Global Modelling of Radio-Frequency Ion ThrustersA. Reeh

A898 Micro-Cathode Matrix Arc Thrusters- A Modified Approach to Micro-Cathode Arc ThrustersK. Daniels

A796 Development of Propulsion Testing and Integration Facilities at Canon ElectronicsK. Masuyama

A549 🌴 Possible electric propulsion schemes based on a combination of RF and DC dischargesI. Zadiriev

17.3

0

A840 Research and develop-ment of radio-frequency cathode-neutralizerP. Smirnov

A884 An energy-dispersive mass spectrometer for electrospray propulsion diagnosticsN. Ford

A655 SITAEL HT100 Thruster, Full Ground QualificationT. Misuri

A216 Performance of a 100-Watt Radial Scaled Thruster with Anode LayerA. Olano Garcia

A699 Three-dimensional simulation of ion thruster plume-spacecraft interaction using EX-PWSH. Zheng

A656 Inter-Laboratory Comparison: Tests of a single thruster in two different facilities, on two different thrust balancesF. G. Hey

A564 🌴 Experimental Study of Traveling Wave Plasma Acceleration and Optimization of Magnetic Field Structure for Electrodeless RF Plasma ThrusterY. Oshio

17.4

5

A477 CNT-based cold electron source for space applica-tions on nano-satellitesP. Laufer

A825 Development status of SITAEL’s 20kW class Hall thrusterT. Andreussi

A527 Design and performance test of the BEHT200 low power hall thrusterY. Hu

A491 Studying the formation and neutralization of an ion thruster plume with EP2PLUSJ. Perales-Díaz

A653 University of Michigan’s Upgraded Large Vacuum Test FacilityE. Viges

A572 🌴 The Transport Character of the Field Reversed Configuration Plasmoid in the Field Reversed Propulsion ThrusterL. Lijuan


Mon

day






Innovative Concepts


18.0

0

A885 SITAEL’S HT400 Hall-Effect Thruster for Constellation ApplicationsT. Misuri

A410 Mechanism Behind the Dependence of Thrust on Facility Backpressure and Implications on the Operation of the SPT-140 Onboard the Psyche MissionI. Mikellides

A804 Theoretical and Experi-mental assessment of Ion Extraction phenomenaM. Mallon

A321 Experimental Study on Ignition Reliability of Pulsed Plasma ThrustersX. Liu

A847 Improved Pumping Speed of Custom Cryopumps for Electric Propulsion Vacuum FacilityM. Crofton

A766 🌴Design of an Experiment for Com-pression and Nozzle Expansion of a Field-Reversed Configuration for Advanced Space PropulsionP. Turchi

18.1

5

A506 Electric Propulsion Activities at Apollo Fusion Inc.—Design, Develop-ment, and Qualification of a Low Power Hall Thruster SubsystemJ. Delgado

A714 Impact of Facility Pressure on the Wear of the NASA HERMeS Hall ThrusterJ. Frieman

A834 Development of a 3D ion optics modelling codeS. Centola

A536 The study on the lifetime of the micro cathode arc thrusterJ. Geng

A785 🌴 Electromagnetic Propulsion Using Non-Ionized Dipole GasesM. Micci

18.3

0

A193 The 12.5 kW Hall Effect Rocket with Magnetic Shielding (HERMeS)R. Hofer

A630 Data-driven Models for the Effects of Background Pressure on the Operation of Hall ThrustersM. Byrne

A854 Neutral Density Simulation in the Grid Region of Ion Thrusters using the ffx Ion Optics CodeJ. Williams

A661 Influence of Insulator Geometry on Vacuum Arc Thruster LifetimeM. Laterza

A848 🌴 Low-Field Mode Transitions in a Spiral-Antenna Helicon ThrusterJ. Little

18.4

5

A266 A 30-kW Class Magneti-cally Shielded Nested Hall ThrusterS. Cusson

A664 Test Results of ExoTerra's Halo Electric Propulsion ModuleM. Vanwoerkom

A169 Predicting Pulsed Plasma Thruster Performance with Deep Recurrent NetworksP. Shaw

A852 🌴 Laboratory demonstration of a bidirectional helicon plasma thruster for space debris removalK. Takahashi

19.0

0

A713 Variation in Ion Acceleration Character-istics of the HERMeS Hall Thruster during Magnetic OptimizationW. Huang

A893 Pulsed Plasma Acceleration Modeling in Detonation and Deflagration ModesK. Polzin

A933 🌴 Lodine as propellant for electric propulsion: optical measurements of I density and temperature, comparisons to a global modelF. Marmuse

Session End

Monday

TUESDAY

Areas


Analytical Modeling



Diagnostics


Mission Analysis

Systems Analysis

Development

Flight Experience

Other


Tues

day


Field Emission / Colloid Thrusters


Innovative Concepts

Power Processing Developments

Thruster Concepts


09:0

0

A628 Experimental characterization of the attachment length in orificed hollow cathodesP.-Y. Taunay

A213 Quantitative mapping of the mechanisms affecting electros-pray thruster lifetimeA. Collins

A492 Development of a 5kW Class Hall ThrusterC. Mullins

A904 SITAEL’s HT5k LL Magnetically -Shielded Hall Thruster TestsT. Andreussi

A355 🌴 Physics Principles for Opti-mization of HEMP-thruster using PIC simulationsP. N. Maya

A108 🌴 Analysis of Distributed Energy Release Charac-teristics in an Ablative Pulsed Plasma ThrusterL. Yang

A361 Directed-Energy Propulsion Architecture for Deep-Space Missions with Characteristic Velo- cities of Order 100 km/sJ. Polk

A110 Hight-efficiency discharge power supply for engine system with Hall ThrusterO. Petrenko

A242 Digital Filtering of Electric Thruster Time Domain Radiated EmissionsN. Rongione

09.1

5

A663 Two-Photon Absorption Laser Induce Fluorescence (TALIF) of Neutral Xenon Density in a Barium Oxide Hollow Cathode PlumeT. Wegner

A368 Resolving electrospray emission modes using high-speed current measurementsN. Uchizono

A140 Development of a 1.5KW High Specific Impulse Magnetic Shielded Hall ThrusterA. Mishra

A879 SITAEL’s Magnetically Shielded 20 kW Hall Thruster TestsT. Andreussi

A504 🌴 Key factors affecting the parameters of inductive RF ion thruster in continuous and pulsed operating regimeE. Kralkina

A457 🌴 Preparation of space experiment to study ionosphere using pulsed plasma injectors with increased power aboard the ISSA. Bogatyi

A458 Hybrid Electric Propulsion System on the Basis of SPT and PPTM. Kazeev

A187 Study of Operation of Power and Propulsion System based on Closed Brayton Cycle Power Conversion Unit and Electric PropulsionA. V. Karevsky

A521 Direct thrust measurement of a vacuum arc thrusterJ. Jarrige

09.3

0

A689 Time-Resolved Electron Density and Temperature Measurements in a Hollow Cathode Discharge by Cavity Enhanced Thomson ScatteringA. Friss

A571 Spatially-Resolved Electrospray Plume Current and Mass Flux Measurements and AnalysisA. Thuppul

A274 High Throughput 1.5 kW Hall Thruster for SatcomsS. Zurbach

A591 Preliminary tests of HIKHET laboratory model at IPPLMJ. Kurzyna

A678 🌴 Global model of a magnetized ion thruster with xenon and iodineR. Lucken

A497 🌴 Investigation on the Discharge Arc Behaviour of an Asymmetric Electrodes Pulsed Plasma ThrusterZ. Zhang

A508 Optimization of Electric Propulsion System Param-eters of LEO SpacecraftsM. Kazeev

A270 Electric Propulsion Mission Design with Minimal Solar Cells Radiation DegradationA. Starchenko

A595 Mechanically amplified milli-Newton thrust balance for RF-thrustersM. Wijnen

09.4

5

A760 5-100 A LaB6 Hollow Cathodes for High-Power Hall ThrustersG. Becatti

A892 Characterization of Electrospray Thruster Electrode Overspray and BacksprayC. Marrese-Reading

A901 Development of the High Voltage Hall Accelerator Propulsion SystemH. Kamhawi

A735 Preliminary Tests of UK90 Hall Thruster with Internal Hollow CathodeU. Kokal

A831 🌴Investigation on Alternative Propellants for Gridded Ion EnginesN. Fazio

A533 🌴 Plume and current-volt-age characterization of the micro-Cathode Arc ThrusterY. Qin

A424 Crosscutting High Apogee Refueling Orbital Navigator (CHARON) for Active Debris RemovalJ. Slough

A190 High Efficiency Auto Resonant Converter Anode Power Supply Design, Development TestingM. Richards

A715 Development of the SPACE Lab Thrust Stand for Millinewton Thrust MeasurementP. Thoreau

10.0

0

A427 Mode Transition in a LaB6 Hollow Cathode for Electric Propulsion Systems for Small SatellitesG.-C. Potrivitu

A909 Microfluidic and materials improvements in the ion Electrospray Propulsion SystemB. Kristinsson

A282 Overview of the Ascendant Sub-kW Transcelestial Electric Propulsion System (ASTRAEUS)R. Conversano

A343 Effects of Thrust Noise on Drag-Free and Attitude Control SystemK. Cui

A862 🌴 Integrated Vlasov-Fully Kinetic PIC Simulations of Plasma PlumesC. Cui

A576 🌴 Temporal and Spatial Ion Velocity Distributions of a Short-pulse Coaxial Laser-assisted Pulsed Plasma ThrusterT. Mikami

A462 Concept Study of Air-breathing HeliconThrust In an Ultra-low-OrbitQ. Y. Ren

A280 Deep Space Power Processing Unit for the Psyche MissionS. Malone

A578 Self-calibration Laser Induced Fluorescence technic in Electric Propul-sion plasma diagnosingX. Yang

10.1

5

A428 Systematic Testing of Improved Designs of Miniaturized LaB6 Hollow Cathodes for Electric Propulsion Systems for CubeSats and Small SatellitesG.-C. Potrivitu

A283 Development Acceptance Testing of the Thruster Compo-nent of the Ascendant Sub-kW Transcelestial Electric Propulsion System (ASTRAEUS)R. Conversano

A377 Mini-CHT powered Formation Flying Mission for Magnetic Reconnection Research in SpaceJ. Simmonds

A882 🌴 Influence of Hollow Cath-ode design parameters on Ring Cusp Discharge Chamber performancesF. Cannat

A476 🌴 PETRUS 2.0 PPT and its CubeSat-size PPU: Testing and Characteri-zationC. Montag

A485 Ultra-low- orbit Space-craft Long Term SustainedH. Zhao

A346 Designing, Manufacturing and Testing of Power Processing and Control Unit for a 1.5 kW Hall Effect ThrusterS. Neugodnikov

A863 Laser ablation plasma diagnostics for electro-static accelerationA. Hamada

10.3

0

A369 Lithium Hollow Cathode for a Very High Isp Interstellar Precursor Ion ThrusterD. Goebel

A873 Development of a low power HEMP Thruster EV0R. Heidemann

A651 The Application of an Advanced Electric Propulsion System on the NASA Power and Propulsion Element (PPE)D. Herman

A409 Design and Implemen-tation of a High Voltage Supply for Gridded Ion Thrusters using model- based control algorithmsC. Roessler

A623 Active Wave Injection Diagnostic for Plasma Dispersion Relation MeasurementsS. Rojas Mata

10.4

5

A371 High Current Hollow Cathode for the X3 100-kW Class Nested Hall ThrusterG. Becatti

A878 HT5k Development Status, Future Activities and Market OpportunitiesT. Andreussi

A419 REGULUS: Know-How Acquired on Iodine PropellantD. Pavarin

A538 Torsional Balance Thrust Measurement Techniques for Small RF ThrustersC. Cretel

11.0

0

Conference Tour

Tuesday

WEDNESDAY

Areas


Analytical Modeling



Diagnostics


Mission Analysis

Systems Analysis

Development

Flight Experience

Other


Wed

nesd

ay



Hall Thrusters 1 Hall Thrusters 2 Ion Thrusters Resistojets/ Arcjets

Innovative Concepts


Thruster Concepts


09:0

0

A782 Recent Advances in Low-Current Hollow Cathodes at SITAELD. Pedrini

A139 Dual-Axis Torsional Thrust Stand for Simultaneous Direct Measurement of Thrust and Mass LossM. Gilpin

A906 Qualification Status of the PPS® 5000 Hall Thruster UnitO. Duchemin

A156 Code-to-Code Verification of Stochastic Models for Electric Propulsion Plume SimulationS. Araki

A356 T7 thruster design and performanceJ. Perez Luna

A224 Electrostatic Probe Investigation of Very Low Power Arcjet VELARC in IRS and ESA-ESTEC FacilitiesJ. Skalden

A158 Optimum design for the drive-coil of a 500J inductive pulsed plasma thruster and its numerical evaluationB. Che

A423 RF Power Processing for a VASIMR® SystemJ. Squire

A232 Electromagnetic-PIC simulation of an ECR plasma thrusterJ. C. Porto

09.1

5

A207 Tests of an iodine-fed rf-neu-tralizerP. Dietz

A226 Investigations into multiple emission sites in porous electrospray thrustersC. Tacon

A673 Qualification status of the EP system for Heinrich Hertz satellite (H2Sat)S. Ciaralli

A157 Unified Framework for Hall-Effect Thruster, Plume, and Spacecraft Charging Models to Assess Spacecraft IntegrationS. Araki

A688 T5 Performance, Indus-trialisation and Future ApplicationsP. Randall

A122 An Efficient Ionization Method for Pressure Up To Thousands of PascalsL. Chang

A191 Effects of Collisional-Ra-diative Processes with Relative Drift in Electric Propulsion DevicesR. J. Abrantes

A474 Development of a full bridge series resonant radio-frequency generator for optimized RIT operationJ. E. Junker

A415 Numerical Model of a Magnetically Enhanced Plasma ThrusterM. Magarotto

09.3

0

A896 Ariane Group 5A Neutralizer qualification statusC. Altmann

A445 Development of a Retarding Potential Analyser for Low Density FEEP Thruster Beam DiagnosticsN. S. Mühlich

A599 Development and Performance Test of a 50 W-class Hall thrusterD. Lee

A222 Long-term Scale Characteristics of Low-frequency Oscillation of Hall ThrustersL. Wei

A360 Testing of a 50,000-s, Lithium-fueled, Gridded Ion ThrusterJ. Brophy

A170 The Development and Qualification of the STAR Resistojet System for Telecommunications ApplicationsF. Romei

A248 Electrocoalescence in Ultrasonic Electric Propulsion systemW. He

A512 High Voltage Power Supply for T5 Gridded Ion ThrusterM. Blaser

A426 Development of a PIC-FDTD code for modelling RF plasma dischargeR. Kalampattel

09.4

5

A297 Performance Testing of a Microwave ECR Neutralizer for the X-EPT Gridded Ion Thruster for Telecoms ApplicationsS. Reeve

A566 Two-dimensional plasma plume density characterisation of the IFM Nano ThrusterS. Keerl

A461 Design and preliminary testing of a laboratory low power Hall ThrusterM. Panelli

A235 Study of Xenon Wall Accommoda-tion Model and Background Flow During Hall Thruster Ground TestG. Ito

A640 HEMPT Ion Thruster Operation with Krypton PropellantA. Genovese

A786 A 17.8-GHz Ammonia Microwave Electrothermal Thruster for CubeSats and Small SatellitesM. Micci

A259 Water as an Alternative Propellant for a Next Generation Plasma Propulsion SystemA. Schwertheim

A567 Design and Manufactur-ing of Control Unit for low and medium power Hall Effect ThrusterS. Neugodnikov

A460 Simulations of magnetized plasma thruster plumesF. Cichocki

10.0

0

A148 Improving EP device performance and lifetime with plasma-robust surface architecturesC. Huerta

A260 MEMS FEEP Thrusters – Minia-turised Liquid Metal Ion Source using Glass CapillariesM. Tajmar

A832 Preliminary design of a low-pow-er Hall ThrusterC. Groll

A263 Numerical Investigations of Background Pressure Effects and Channel Erosion in the SPT-140 Hall Thruster for the Psyche MissionA. Lopez Ortega

A811 Development and testing of the NPT30 ion iodine thrusterJ. Martínez

A393 Lifetime Investigations of an Additively Manufac-tured High-temperature Resistojet Heat Exchang-er from TantalumM. Robinson

A265 Multifluid FRC Formation Modeling with Relative Drift Corrected Collision-al-Radiative ProcessesR. Lilly

A575 Development of High Efficiency Power Processing Unit for Hall ThrusterA. Tsybulnyk

A564 Investigation of the Circuit and Ablation Model for a Vacuum Arc ThrusterS. Bai

10.1

5

A172 LaB6 hollow cathode work function enhancement: insight into the chemical processesP. Guerrero

A362 Development, Production, and Testing of the IFM Nano FEEP ThrusterT. Schönherr

A634 Development and Characteri-zation of a Miniature Hall-Effect Thruster using Permanent MagnetsN. Gondol

A247 Numerical Simulations of AFRL EP/TEMPEST experiment using the Thermophysics Unified Research Framework (TURF)L. Brieda

A383 Development of 50 W class RF gridded ion thrusterD. Q. Pham Tran

A403 Failure analysis of endurance tested 316L stainless steel Super High Temperature Additive Manufactured Resistojet (STAR) C. Ogunlesi

A324 Numerical investigation of “Detachment Cone” in the magnetic nozzleZ. Chen

A584 Power Processing Unit Activities at Thales Alenia Space in BelgiumE. Bourguignon

A573 Numerical Analysis of Plasma Acceleration Driven by Loop Coil in Electrodeless ThrusterY. Yamakawa

10.3

0

A245 Plasma model and experimental investigation of a hollow cathode neutraliserA. Gurciullo

A675 The IFM Micro FEEP thruster: a modular design for smallsat propulsionL. Grimaud

A375 Miniaturized Cylindrical Hall ThrustersJ. Simmonds

A237 Study on Feed System of Iodine Cusped Field ThrusterH. Liu

A446 Development Status of Microwave-ion Thruster M5 for Small and Micro SatellitesK. Zhu

A631 Effect of structure characteristics on start-up process of an Arcjet thrusterY. Shen

A330 Numerical Simulations of the Plasma Discharge in an Helicon Plasma ThrusterJ. Zhou

A696 Flying Capacitor Multilevel Converters for use in the ASTRAEUS Anode Power SupplyA. Barchowsky

A647 Optimization of electro-thermal microwave plasma thruster for nanosatellitesS. Ivanov

10.4

5

A301 Hollow cathode thermal model-ling and self-consistent plasma solution: two step neutralization modellingP. Guerrero

A686 The ESA Earth Observation Pro-gramme activities for the design, development and qualification of the mN-FEEP thrusterL. Massotti

A465 Investigation of the possibility to develop competitive small power stationary plasma thruster (SPT)V. Kim

A285 Influence of plume magnetic field on discharge performance of Hall thruster under internal and external cathode position studied by particle-in-cell simulationX.-F. Cao

A900 The Development and Test of a Dual Mode Micro Microwave Gridded Ion Thruster for Orbit Raising and Attitude KeepingA. Vafabakhsh

A560 Research on Micro Impulse Measurement Technology for Micro Cathode Arc ThrusterX. Liu

A728 RAFAEL's Compact Power Supply Unit (PSU) for an Affordable Electric Propulsion System (EPS)D. Lev

A666 Nanosecond Pulsed Micro-Plasma Thruster for Small SatellitesN. Rogers

Wednesday


Wed

nesd

ay




Innovative Concepts


Thruster Concepts


11.0

0

A331 An Axisymmetric Eulerian- Kinetic Solver for Simulation of Hollow CathodesA. R. Vazsonyi

A805 CLIMB: Exploration of the Van Allen Belt by CubeSatsC. Scharlemann

A836 Overview of NASA’s Solar Electric Propulsion ProjectP. Peterson

A294 EP plasma plume in orbit: Diag-nostics and analysis correlationJ. Laube

A652 Performance Testing of the X-EPT Microwave ECR Gridded Ion Thruster for Telecoms ApplicationsD. Hoffman

A225 Development Progress of an Adaptable Deorbit System for Satellite ConstellationsJ. Skalden

A590 Interaction of Droplets in Electrospray PlumesM. Davis

A729 Rafael's Power Process-ing Unit (PPU) for Electric Propulsion SystemsD. Lev

A795 Numerical Simulation and theoretical analysis of Particle Acceleration in Traveling Magnetic Field ThrusterH. S. Kumar

11.1

5

A452 A Plasma Model for Orificed Hollow CathodesM. Panelli

A724 Recent flight data of the IFM Nano Thruster used for LEO orbit raisingD. Krejci

A779 Development of low-power micro cylindrical hall thruster “SCHT-1”T. Ikeda

A639 Coupling of an all-electric spacecraft with its plasma plume and its environmentS. Hess

A143 Development of the Miniature Xenon Ion Thruster with Hollow Cathode OperationS. Samples

A390 Performance Theory and Development of a Resistojet Based Hybrid Electro-Chemical ThrusterG. Coral

A633 PIC/fluid/wave simu-lations of the plasma discharge in an ECR plasma thrusterA. Sánchez-Villar

A888 AIRBUS DS PPU qualification status for HET, GIT and New Space TechnologiesF. J. Pintó Marín

A609 Discrete Boltzmann Modeling of Atmospheric Pressure Plasma JetJ. Song

11.3

0

A914 Validation of a drift diffusion model for a hollow cathodeS. Gabriel

A828 UWE-4: In-orbit characterization of the NanoFEEP propulsion systemA. Kramer

A702 Development of BUSTLab Low Power Hall Thruster for Use at LEO Mini-Satellite SystemsU. Kokal

A833 Simulation of plasma plume experiments with Hall Thrusters: on-ground chamber effects on measurements and extrapolation to in-flight situationP. Sarrailh

A558 Development of 5 kilo-watts electric propulsion system on Satellite SJ-20G. Jun

A913 Development of a High Voltage Power Process Unit for a CubeSat Electrospray ThrusterC. Ma

A818 Effect of the initial electron distribution function in magnetic nozzle expansionsS. Correyero Plaza

11.4

5

A781 A One-Dimensional model for Hollow Cathode Orifice lifetime predictionF. Bosi

A895 LISA Colloid Microthruster Technology Development Plan and ProgressJ. Ziemer

A856 Small Permanent Magnets Hall Plasma Thruster Development for Micro and Nano SatellitesJ. Ferreira

A858 Thruster Plume and Spacecraft Interaction Analysis by 3D Electrostatic Code for 4.5-kW-Class Hall ThrusterT. Muranaka

A754 NEXT-C Flight Ion System Development StatusJ. Fisher

A930 13kW Advanced Electric Propulsion System Power Processing Unit DevelopmentE. Soendker

A744 A 3D Numerical Study of Arcjet Thrusters: Effect of Electrode Configuration on Performance of Arcjet thrusterN. Hari Prasad

12.0

0

Lunch Break

A627 Experimental investigations and performance optimisation of the Halo thrusterS. Masillo

A912 High Power Ion Propulsion System for the Double Asteroid Redirection Test MissionJ. Fisher

A937 Research on a controlled high voltage power supply for Power Processing UnitQ. Kang

12.1

5

A464 Development of compact high efficiency RF generator for inductive coupled plasma sourcesA. Surminskii

13.3

0 Plenary Lecture AudimaxLEO

15.0

0

A783 Numerical modeling and incoherent Thomson scattering measurements of a 5A cathode with LaB6 emitterL. Garrigues

A196 Droplets emission from FEEP and colloids thrusters: modelling of droplets dynamics and interac-tion with spacecraft bodyM. Villemant

A336 The research of the modified SPT-70 thruster parameters and characteristicsA. Markov

A318 Coupled Simulation of Two-Di-mensional Hybrid Hall Thruster ModelsR. Kawashima

A668 The Analysis of Parameter Sensitivity of Electron backstreaming failure mode for 3-grid system ion thrusterY. Jia

A520 Numerical Investigation of Micro-Cathodic Arc Thruster Lifetime using the PIC-DEM MethodL. Brieda

A174 Design and preliminary experiments of the prototype of a 500J inductive pulsed plasma thrusterX. Li

A198 Electrodeless Helicon Plasma Thruster Employing Additional Electromagnetic Acceleration MethodT. Furukawa

Wednesday


Wed

nesd

ay




Innovative Concepts

Thruster Concepts

HS6 SR5 SR6 SR7 HS5 SR4 HS3 HS2

15.1

5

A865 Comparisons between Particle Simulation using IAT Growth Model and Plume Measurements of LaB6 Hollow CathodeK. Kubota

A317 Uncertainty Quantification of Electrospray Thruster Array LifetimeB. Jorns

A660 I2HET: Development of an Iodine-Fed Hall Effect ThrusterM. M. Saravia

A518 Hybrid modeling of the anoumalous transport inside Hall thrustersA. Alvarez Laguna

A680 Surface Modification of Pyro-lytic-Graphite Grids for an Ion thrusterY. Matsunaga

A837 Numerical Rebuilding of Very Low Power Arcjet Thruster VELARC in Test Facilities at IRS and ESA-ESTECP. P. Upadhyay

A178 The Status of the VASIMR(R) Engine Development ProgramM. Carter

A537 An Experimental Study of Thrust Dependence on Magnetic Field in an Electrodeless Inductive Plasma AcceleratorA. Tatsuno

15.3

0

A874 Fluid model of a Hollow Cathode dischargeX. Chen

A526 Colloid Thruster Plume Simula-tions Using a Particle-Particle ModelJ. Wang

A838 Simulation of an Adaptable Hall ThrusterN. Proulx

A648 Multiscale Hybrid Modeling of Unconventional Hall ThrustersM. Laterza

A722 Uncertainty Quantification of Modeled Electron Backstreaming Failure for the NEXT Ion ThrusterJ. Yim

A562 A Chemically Augmented Arcjet Thruster with Exotic PropellantsM. Tsuchiya

A583 Advanced and nanostructured materials for electric propulsion and small satellitesI. Levchenko

A596 Development and Character-ization of the Helicon Plasma Thruster Prototype HPT-03J. Navarro-Cavallé

15.4

5

A658 Numerical and Experimental Investigation of Different Heater Designs for Lanthanum Hexabo-ride Hollow CathodesU. Kokal

A530 Effect of Aprotic + Protic Mixtures on Electrospray Droplet FragmentationD. Levin

A902 Performance, Plume, Stability, and Wear Characterization of Three Alternate Magnetic Field Topologies in the Hall Effect Rocket with Magnetic ShieldingH. Kamhawi

A358 The impact of the SPT-140D parameters and lifetime characteristics change on its thermal modeP. Chubov

A827 Endurance Testing of Iodine BIT-3 RF Ion Propulsion SystemM. Tsay

A703 Effect of adding water to propellant of a DME arcjet thrusterT. Tachibana

A646 Operation and Performance of a Fully-Integrated ion Electrospray Propulsion SystemB. Kristinsson

A608 XMET: Testing of an Argon/Xenon Microwave Electrothermal ThrusterT. Baxter

16.0

0

A144 🌴 Porous Materials for Long Life and High Performance Electric PropulsionG. Li

A830 Development of an Electrospray Source Model for Kinetic Plume ModelingE. Petro

A637 Characterisation and Performance Comparison of a Low-Power Hall-Effect Thruster and an Advanced Cusp Field Thruster with Multiple Noble GasesM. Vaupel

A281 Plasma Simulations for the Assessment of Pole Erosion in the Magnetically Shielded Miniature Hall Thruster (MaSMi)A. Lopez Ortega

A907 Modeling Ion Optics Erosion in the NEXT Ion Thruster Using the CEX2D and CEX3D CodesJ. Polk

A742 Direct Inertial Electrostatic Confinement Propulsion at Low Power LevelsM. Winter

A855 Performance improvement of a magnetic nozzle helicon plasma thrusterK. Takahashi

16.1

5

A153 🌴 Development of Low-Volt-age-Driven Propellantless Cathodes with High-Current Density Based on Graphene-Ox-ide-Semiconductor StructureR. Furuya

A559 🌴 Study on Performance of Ionic Liquid Electrospray Thruster in Atmosphere and Vacuum EnvironmentY. Guo

A752 Preliminary Evaluation of Anode-Layer-Type Hall Thruster Performance Using RF Plasma Cathode with Pulsating Boost Chopper CircuitK. Nagamine

A364 Particle-In-cell / fluid simulations of a Hall effect thruster account-ing for plasma wall interactionsW. Villafana

A761 Experimental demonstration of thrust vectoring magnetic nozzle with multi-axis thrust measurement systemM. Edamoto

A867 Cubesat Test Platform for miniaturized electric propulsion system verification campaignF. Stesina

16.3

0

A214 🌴 Radio Frequency Microdischarge NeutralizerF. Filleul

A622 🌴 One to One Comparison of Chemically Energetic and Inert Electrospray PropellantsC. Lyne

A771 Effects of Pulsating Boost Chopper Power Supply on the Performance of TAL-type Hall ThrusterK. Hasegawa

A478 The Sputtering Mechanism of Keeper Electrode in Hall ThrusterJ. Chen

A815 Enabling High-Energy Missions with Nanosatellites by Using Ablative Pulsed Plasma ThrustersP. Gessini

16.4

5

A788 🌴 High-Speed Transient Character-ization of the Busek BET-300-P Electrospray ThrusterD. Courtney

A563 Impact on Performance and Erosion in Hall Thruster using Argon and Xenon propellantJ. Yamasaki

A534 Numerical Prediction of Wall Erosion Morphology on Hall ThrustersN. Wu

A920 The operation of a low-power cylindrical Hall thruster with zinc as the propellantC. Ryan

17.0

0

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

Session End → Gala Dinner beginning 18.30

Wednesday

THURSDAY

Areas


Analytical Modeling



Diagnostics


Mission Analysis

Systems Analysis

Development

Flight Experience

Other


Thur

sday



Hall Thrusters 1 Hall Thrusters 2 Ion Thrusters MPD Thrusters Innovative / Advanced Propulsion Concepts

Thruster Concepts


09:0

0

A249 🌴 Comparison of transient behavior in a 20 A hollow cathode in a 9 kW Hall thruster and a stand-alone configurationM. Georgin

A600 Electric Propulsion Develop-ments at Rafael in 2019D. Lev

A115 Use of Real-Time Spectrum Analysis for EMI Characterization of the SAFRAN PPS5000 Hall ThrusterW. Tighe

A487 Oscillation analysis in Hall thrusters with 2D (axial-azimuth-al) Particle-In-Cell simulationsT. Charoy

A127 Electric Propulsion Direct-Current Current Transformer (EPDCCT): Design and Experimental ValidationC. Volkmar

A493 Magnetic Field and Current Density Probe for Steady State AF-MPD ThrustersA. Behnke

A164 Evaluation of anomalous resistiv-ity in a low power magnetic nozzleS. Hepner

A188 Comparison of waveguide-cou-pled and coaxial-coupled ECR magnetic-nozzle thruster using a thrust balanceS. Peterschmitt

09.1

5

A359 🌴 Pulsed Electron Beam Extraction from a Hollow CathodeB. Karadag

A592 The Ariane Group Electric Propulsion Program 2019-2020H. Leiter

A793 Life Estimation of Hall Thrusters using Multi Spectral ImagingH. Gole

A501 Enhancing Hall Effect Thruster Simulations with Deep Recurrent NetworksP. Shaw

A287 Non-intrusive measurements of microwave ion thruster by two photon absorption LIF and laser Thomson scatteringR. Tsukizaki

A551 Simultaneous Measurement of Cathode Surface Temperature Distribution and Plasma Spatial Distribution in Self-Field MPD ThrusterS. Tauchi

A199 Experimental Validation and Performance Measurements of an ECR Thruster Operating on Multiple PropellantsR. Moloney

A219 Optimization of a Low Power ECR Thruster Using Pulsed Power and Frequency Mixing TechniquesB. Wachs

09.3

0

A430 🌴 Mechanism Analysis of Cathode Low Frequency OscillationZ. Ning

A926 Overview of Busek EP ThrustersV. Hruby

A408 Terahertz Time-Domain Spectroscopy as an Electric Propulsion Plasma DiagnosticN. Brown

A732 Data-Driven Modeling for Nonlinear Dynamics of Phys-ical Phenomena in Hall Effect ThrustersC. Greve

A337 Estimation of Erosion Rate for Surface Material on HAYABUSA2 by Measurement of Backflow Ions from 10-cm-class Ion ThrusterT. Muranaka

A918 Thrust Performance and Cathode Temperature Evaluation of MW Class Quasi-Steady MPD ThrusterS. Tonooka

A261 The SpaceDrive Project – EMDrive Thrust Measurements and AnalysisM. Tajmar

A267 Development of the hall effect hollow cathode thrusterL. Chenguang

09.4

5

A603 🌴 Replacing keeper orifice plate with emissive material: emission mechanisms and impacts on hollow cathode dischargeT. Meng

A861 Application of Helium Line Intensity Ratio Spectroscopy to Xenon plasma in Penning dischargeH. Sekine

A792 Data-Driven Modeling for Nonlinear Dynamics of Phys-ical Phenomena in Hall Effect ThrustersD. Bilyeu

A348 A novel optical line-ratio method for measuring the electron parameters in the discharge chamber of xenon ion thrustersX. Zhu

A310 The Experimental Performances of the 100kW MPD Thruster with Applied Magnetic FieldY. Cong

A262 The SpaceDrive Project – Over-view of Revolutionary Propulsion Efforts at TU DresdenM. Tajmar

A363 Diagnostics and testing facilities for ionic liquid electro-spray thrusters at the Air Force Research LaboratoryD. Eckhardt

10.0

0

A604 🌴 Applicability of electride materials for hollow cathodesM. Reitemeyer

A516 Hall Thruster Plume Measure-ments of Time Resolved Ion EnergyT. Kerber

A579 Analysis of the plasma discharge in a Hall thruster via a hybrid 2D codeP. Fajardo

A396 Optical plasma diagnostics for radio-frequency ion thrustersB. Nauschütt

A314 Cathode Ablation Performance of Applied-Field Magnetoplasma-dynamicG. Wang

A271 Plasma Jet Pack (PJP) TechnologyA. Blanchet

A417 REGULUS: Iodine Fed Plasma Propulsion System for Small SatellitesD. Pavarin

10.1

5

A649 🌴 Ampere-Level C12A7 Cathode Operation with Initial Testing of Heaterless IgnitionM. Mcdonald

A308 Electron cross-field transport mechanism observed under the azimuthally inhomogeneous neutral supply in a Hall thrusterJ. Bak

A613 Boundary conditions for a two-dimensional direct kinetic simulation of a Hall thrusterA. Raisanen

A503 Two-Photon Laser-Induced Fluorescence Diagnostics of a Radiofrequency Ion Thruster: Measurements in Xenon and KryptonC. Eichhorn

A401 Anode Power Deposition in an AF-MPDT with Two Unique Magnetic FieldP. Wu

A279 Thruster Performance Results for the 200 kW Peristaltically Driven Plasma AcceleratorJ. Slough

A498 XMET: Design and early testing of a xenon microwave electrother-mal thrusterD. Staab

10.3

0

A690 🌴 Hollow Cathode Technology for Low Power Electric Propulsion ApplicationsW. Ohlinger

A449 On-board Plasma Plume Diagnostics for ETS-9 All-electric SatelliteK. Kinefuchi

A619 Operation of a Low Power Hall Thruster with a Shielded Magnetically ConfigurationL. Garrigues

A525 Development of a Collisional-Ra-diative Model for Plasma Thruster Optical DiagnosticsM. Celik

A544 Design of Water MPD ThrusterA. Kakami

A290 Characterisation of a Rotational Thrust Balance for Propellantless Propulsion Concepts Utilizing Magnetic Levitation with SuperconductorsO. Neunzig

A638 Direct thrust measurements and design upgrade of an ECR thruster operating on water propellantD. Staab

10.4

5

A723 🌴 Hollow Cathode Operation with Time-Varying CurrentsJ. Polk

A252 Significant ion acceleration of Xe ions outside the discharge channel in cylindrical Hall thruster plasmas observed by laser induced fluorescenceG. Doh

A642 Influence of Magnetic Field Strength on Narrow Channel Hall Thruster Discharge Operating at Very Low PowerI. Kronhaus

A611 Evaluation of Faraday Probes towards its Standardisation for Electric Propulsion TestingQ. Koch

A585 Current Advances in Optimiza-tion of Operative Regimes of Steady State Applied Field MPD ThrustersA. Boxberger

A292 Influence of cathode grid dimen-sion on discharge characteristics of IEC thrusterY.-A. Chan

A822 Status of HEMPT-NG development programme at Thales UlmS. Weis

Thursday


Thur

sday




Thruster Concepts


11.0

0

A776 🌴 Characterization of a 100 A-class LaB6 hollow cathode for high-power Hall thrustersS. Mazouffre

A246 Hall Thruster Near-Field Plume Characterization Through Optical Emission SpectroscopyM. Nakles

A720 Numerical studies of the ExB electron drift instability in Hall thrustersF. Taccogna

A618 Test Facility for EMC-Character-ization of Electric Thrusters in Operation using an evacuated Reverberation ChamberR. Thüringer

A588 Experimental study of the discharge characteristic in AF-MPDT ignitionY. Wang

A333 High-Specific-Impulse Operation in Diverging Magnetic Field Electrostatic Thrusters with Argon PropellantD. Ichihara

A875 H2020 MINOTOR: Magnetic Nozzle Electron Cyclotron Resonance ThrusterD. Packan

11.1

5

A845 🌴 Total Sputter Yield Character-ization of Various Spacecraft MaterialsJ. A. Young

A515 Development and Validation of a Time-Resolved Ion Energy Distribution DiagnosticM. Baird

A437 3D simulation of rotating spoke in a wall-less Hall thrusterK. Matyash

A738 Determination of the Beam Divergence of a Gridded Ion Thruster Using the AEPD PlatformC. Bundesmann

A759 Characterization and Improve-ment of Thrust Balance for High Power Applied Field MPD ThrustersG. Herdrich

A382 Metallic Ion Thruster using Mag-netron E-Beam bombardmentK.-Y. Chen

A897 HiperLoc-EP: A new approach for SmallSats Electric PropulsionJ. Stark

11.3

0

A929 🌴 Additively Manufactured Hollow Cathode Keepers with Integral Radiation ShieldingM. S. Mcdonald

A734 HK40 Hall Thruster Plume Plasma Measurements with Retarding Potential Analyzer, Faraday Probe and Langmuir ProbeU. Kokal

A347 Study of the Electron Cyclotron Drift Instability inside Hall Effect Thrusters with a fluid codeV. Joncquieres

A777 Planar probe array for bidimen-sional mapping of the ion flux profile of a miniaturized ion thrusterL. Habl

A385 Thrust Generation in Electro-static-Magnetic-Hybrid Plasma ThrusterA. Sasoh

A941 Development of the Xenon Cold Gas Thruster to Support All-Electric Propulsion MissionsI. Johnson

11.4

5

A155 🌴 Onset criteria for the plume mode oscillation in hollow cathodesM. Georgin

A387 Study of two different discharge modes in Hall thrusterI. Khmelevskoi

A726 Development of 1D Magneto-stat-ic Two-Fluid Plasma Simulation of a Hall Effect ThrusterR. Sahu

A167 Near Field Probe Measurements in the Plume of a NEXT Ion ThrusterN. Arthur

A475 Design and Performance Test of a RF Plasma Bridge NeutralizerD. Spemann

12.0

0

A667 🌴 The neutral gas properties in orifice hollow cathode before its ignitionY. Jia

Lunch Break & Poster Session

14.0

0 Plenary Lecture AudimaxBEPI Colombo

15.0

0

A823 BEPI- Colombo Electric Propulsion in MercuryR. Velasco Valencia

A841 Non-intrusive Characterization of the Wear of the HERMeS Thruster Using Optical Emission SpectroscopyT. Gray

A733 Coupling Non-Maxwellian View Factor Model to Octree Based Particle VDF Compression for Accelerated Spacecraft-Plume SimulationR. Martin

A171 Measurement of a Concentric Split-Ring Resonator Microplasma for Miniature Ion EnginesK. Xu

A195 A Novel Laser Ablation Magneto-plasmadynamic ThrusterY. Zhang

A488 Inductive Plasma Thruster (IPT) for an Atmosphere-Breathing Electric Propulsion System: design and set in operationF. Romano

A467 🌴 Performance Analysis of the Capacitively Coupled Radio Frequency ThrusterA. Quraishi

15.1

5

A305 BepiColombo - Solar Electric Propulsion System Operations for the Transit to MercuryC. Steiger

A932 Internal Probe Studies of a Low Voltage Hall ThrusterJ. L. Ross

A880 Particle-In-Cell model of the dynamic of the electrons between the two walls of Hall thrusters including realistic secondary electron emission dataM. Villemant

A175 Design and Experimental Study of an Miniature Ion ThrusterJ. X. Ren

A313 Development of High Power Magnetoplasmadynamic Thrusters in BICE and Beihang UniversityY. Li

A500 Review of Dualmode/Multimode Space PropulsionJ. Rovey

A577 🌴 Proposal and Performance Evaluation of Microwave-Driven In-Tube Accelerator ConceptM. Takahashi

15.3

0

A606 BepiColombo – The Mercury Transfer ModuleH. Gray

A384 Incoherent Thomson scattering investigations of a low-power Hall thruster in standard and magnetically-shielded configu-rationsB. Vincent

A215 Numerical solutions of Density Gradients Instability in a Hall Thruster PlasmasS. Singh

A238 Preparation of Space Experiment with Electric Propulsion System Based on Radio-Frequency Ion Thruster aboard the International Space StationR. Akhmetzhanov

A542 Applied-Field MPD Thruster with High Current Heater-less Hollow CathodeJ. Yamasaki

A552 Interaction of Ultraviolet Light-emitting Diodes and Solid Polymers for Micropropulsion ApplicationsH. Horisawa

A594 🌴 Indirect electrothermal acceleration of a cold gas jet through interaction of an arcjet exhaust flow for space propulsion applicationsY. Arai

Thursday


Thur

sday




Thruster Concepts


15.4

5

A615 BepiColombo – MEPS commissioning activities and T6 ion thruster performance during early mission operationsP. Randall

A617 Characterization and perfor-mance measurements of 40 W-class and 100 W-class Hall thrustersT. Hallouin

A239 Atmospheric Ramjet Thrust Unit on the Base of High-frequency Ion ThrusterM. Suvorov

A872 Development of a 10-30 kW Augmented Field MPD Thruster at SITAELA. Kitaeva

A605 Hybrid Electric Propulsion System based on Water ElectrolysisN. Harmansa

A610 🌴 Informing the design of pure-ion electrospray thrusters via simulation of the leaky-dielectric model with charge evaporationX. Gallud Cidoncha

16.0

0

A824 BepiColombo – A mission overviewN. Wallace

A528 Development Efforts on a Laser Thomson Scattering Diagnostic for Electric Propulsion Applica-tionsT. Matlock

A349 🌴 Microinstabilities and rotating spokes in the near-anode region of a Hall thrusterJ.-P. Boeuf

A240 Characteristics of Radio-Fre-quency Ion Thruster with an Additional Magnetic Field in the Ionization AreaV. Kozhevnikov

A450 Performance of Applied Field MPD Thruster with Various PropellantsS. Ide

A621 Advanced Cusp Field Thruster with a 3D-printed discharge channel - Performance with Iodine and XenonM. Vaupel

A643 🌴 Physics and performance of the Alternative Low Power Hybrid Ion Engine (ALPHIE) for space propulsionJ. González

16.1

5

A494 BepiColombo – MTM and MEPS Integration and VerificationK. Kempkens

A598 Experimental Study on the Influence of Magnetic Field on the Performance of Low-power Hall ThrustersX. Yi

A582 🌴 Experimental characterization and modeling of ID-HALL, a double-stage Hall thruster with an inductive ionization stageÁ. Martín Ortega

A339 Ring Cusp Ion Thruster IT-200PMA. Lovtsov

A669 Thrust Evaluation of a Small-seized SF-MPD ThrusterK. Ueno

A645 100 kW Nested Hall Thruster High Power System Demonstra-tionS. Shark

A775 🌴 Azimuthal Induced Current Formation and Ion Acceleration in an Inductive Radiofrequency Plasma ThrusterH. Sekine

16.3

0

A586 BepiColombo - Solar Electric Propulsion System Test and Qualification ApproachS. Clark

A447 🌴 Performance Evaluation of a 100-W Class Hall ThrusterH. Watanabe

A574 Test Campaign on the novel Variable Isp Radio Frequency Mini Ion EngineM. Smirnova

A870 Plasma Plume Characteristics of Cluster Operation of Self-Field Magnetoplasmadynamic ThrusterY. Murayama

A693 100kW Nested Hall Thruster System DevelopmentJ. Jackson

A829 🌴 Two-dimensional Full Particle-In-Cell Simulation of Magnetic Sails in Formation FlightA. Wada

16.4

5

A770 BepiColombo Solar Electric Propulsion Plasma-Spacecraft Interactions: Comparison of Flight Data with Numerical ModellingF. Filleul

A338 🌴 Design and experimental research of a micro-newton cusped field thrusterM. Zeng

A625 Status of HEMPT Electric Propulsion Flight Hardware for Heinrich Hertz SatelliteA. Lazurenko

A921 Traveling Wave Thruster System DevelopmentD. Cope

A692 13kW Advanced Electric Propul-sion Flight System Development and QualificationJ. Jackson

A903 🌴 An experimental revisit of plasma phenomena on Helicon Plasma ThrustersJ. Navarro Cavalle

17.0

0

A741 Erosion and Lifetime of the Aurora Low-Power Hall Effect ThrusterJ. Makela

A816 🌴 Scaling of spoke rotation fre-quency within an ExB DischargeA. Powis

A797 Exprimental studies on the effect of the magnetic field and the electrical potential inside the water ion thrusterY. Ataka

A329 Research on the 500kW Class Superconducting Strong Magnetic Field High Power Magnetoplasmadynamic Thruster TechnologyC. Zhou

A712 The SpaceDrive Project – Progress in the Investigation of the Mach-Effect-Thruster ExperimentM. Monette

A931 🌴 Development of Dielectrophoretic Force Feeding Subsystem for Liquid Pulsed Plasma ThrusterC. Dobranszki

17.1

5

A298 Pole Erosion Measurements for the Development Model of the Magnetically Shielded Miniature Hall Thruster (MaSMi-DM)R. Lobbia

A352 🌴 Neutral gas instabilities in Hall thrusters, Part I: MeasurementsE. Dale

A806 A Nouvelle Neutralization Concept for RIT-µX Miniaturized Radio Frequency Ion Thruster SystemsH. Leiter

A801 Business Cases and System Architecture for Superconduc-tor-based Applied Field Magneto Plasma Dynamic ThrustersM. La Rosa Betancourt

A774 Development of a deployable vacuum arc thruster system for the post-mission disposal of micro/nano satellitesM. Kim

A365 🌴 RF Power - Plasma Coupling Experimental Results in a Helicon Plasma Thruster PrototypeV. Gómez

17.3

0

A209 Hall Thruster Erosion Meas-urement by Time-Resolved Cavity-Ring Down SpectroscopyY. Egawa

A432 🌴 Driving Low Frequency Oscilla-tions in Hall ThrusterY. Raitses

A808 The RIT 2X High Performance Ion Thruster System Qualification ProgramJ.-P. Porst

A886 Development Roadmap of SITAEL’s RAM-EP SystemT. Andreussi

A940 🌴 A thruster using magnetic reconnection to create a high-speed plasma jetS. Bathgate

17.4

5

A332 Numerical simulation and experimental research on low power Hall thruster with long lifeY. Ding

A889 🌴 Gradient-drift instability as an origin of spokes in Hall thrustersN. Marusov

A842 Charge State Thrust Correction Factor for NEXT: DART MissionM. Crofton

Thursday

BepiColombo


Thur

sday




Thruster Concepts


18.0

0

A341 A 2000 Hours Life Test of a 5 kW Multi-mode High Specific Impulse Hall Thruster HEP-140MFW. Mao

A354 🌴 Neutral gas instabilities in Hall thrusters, Part II: TheoryE. Dale

A844 Deposition Rate Measurements in NEXT Ion Engine Plume for DART MissionJ. Young

A293 Back-vacuum Retarding Poten-tial Analyzer for Investigation of IEC plasma propertiesY.-A. Chan

18.1

5

A749 Prediction of liner erosion and life estimation of Stationary Plasma Thrusters using Machine LearningS. Bhat

A632 🌴 Influence of double-stage operation on breathing oscilla-tions and rotating spokes in the ID-HALL thrusterA. Guglielmi

A853 NEXT Single String Integration Tests In Support of the Double Asteroid Redirection Test MissionR. Thomas

A434 Beam Plasma Expansion of a Helicon Plasma SourceZ. Zhang

18.3

0

A433 🌴 Use of electrostatic probes for characterization of the electron cross-field current in ExB plasmasY. Raitses

A859 Experimental Characterization of the Microwave-Discharge Water Ion Thruster for CubeSatsY. Nakagawa

A448 Modeling and Optical Diagnos-tics of Iodine Fed Helicon Type Thrusters by a Detailed Global Model (DGM)K. Katsonis

18.4

5

A323 🌴 Experimental study on the effect of propellant asymmetrical distribution on plasma potential distribution in a Hall effect thrusterM. Ding

A928 Arclight: a plug-in gridded ion propulsion system for small satellitesP. Bauer

A682 A Detailed Global Model for Modeling and Optical Diagnos-tics of Low Power Propulsion Devices Fed by CO2C. Berenguer

19.0

0

Session End

Thursday

FRIDAY

Areas


Analytical Modeling



Diagnostics


Mission Analysis

Systems Analysis

Development

Flight Experience

Other


Frid

ay

←

Hall Thrusters Mission

SR7 HS2

10.4

5

A543 🌴 Towards Predictive Kinetic Simulations of Plasma ThrustersI. Kaganovich

A411 Electric Propulsion Characterisation for a Stand-Alone Mars CubeSatK. V. Mani

11.0

0

A545 🌴 Fluid modeling of gradient-drift turbulence and transport in ExB plasmasA. Smolyakov

A727 Microsatellite Electric Propulsion System (MEPS) Project Status in 2019D. Lev

11.1

5

A691 🌴 New insights into electron transport due to azimuthal drift in a Hall effect thrusterK. Hara

11.3

0

A569 🌴 Assessment of the thermodynamic and fluid approximations for electrons in plasma thruster plumesY. Hu

11.4

5

A304 🌴 Characteristic Transient Phenomena of Hall Effect ThrustersA. Komarov

12.0

0

A758 🌴 🌴 Plasma instabilities in cross-field configuration: an analysis of the relevance of different modes for electron transportS. Tsikata

12.1

5

A843 🌴 🌴 Experimental Correlation between Anomalous Electron Collision Frequency and Plasma Turbulence in a Hall Effect ThrusterZ. Brown

12.3

0

A718 🌴 🌴 Investigation of cross-field electron transport in a 100-W class Hall Thruster using a full particle-in-cell simulationS. Cho

12.4

5A593 🌴 🌴 Simulation of radial electron dynamics in a Hall effect thrusterA. Domínguez-Vazquez

13.0

0

Technical Visits

Hall Thrusters Ion Thrusters Propellant Storage/ Feed Systems

Mission Diagnostic

SR7 HS5 SR5 HS2 SR6

09:0

0

A665 🌴 Plasma fluctuations measurements in a Hall ThrusterN. Yamamoto

A145 Radio-frequency biasing of ion thruster gridsT. Lafleur

A601 Innovative Xenon/Krypton FMS (Feed Management System) for Electric PropulsionP. Barbier

A192 Development of the Psyche Mission for NASA's Discovery ProgramD. Oh

A773 ESA Propulsion LaboratoryE. Bosch Borràs

09.1

5

A687 🌴 Axial-azimuthal high-fre-quency instability modes in a Hall thruster fluid modelE. Bello-Benítez

A431 M S of the Erosion and Contamination Effects on the CAESAR SpacecraftL. Bermudez

A871 Simulation And Exper-imental Study on Xeon Mass Flow Regulating Characteristics of the Proportional Valve Based on Unimorph Ring-Shaped Piezoelectric ActuatorX. Wang

A244 Electric Propulsion for the Psyche MissionS. Snyder

A374 Three-dimensional Vector Measurement of EP Propellant Flow within a Vacuum ChamberY. Nakayama

09.3

0

A454 🌴 Effect of magnetic field configuration on discharge characteristics in permanent magnet thrusters with cusped fieldS. Liang

A507 A global performance model of Gridded Ion ThrustersE. Ahedo Galilea

A400 Development of Porous-Metal-Restrictor Based Xenon Flow Control ModulesG. Hang

A654 Sitael HT100 Missions: uHETSAt and PLATiNOT. Misuri

A517 In-situ microscopy of ion-induced erosion of plasma-facing surfacesA. Ottaviano

09.4

5

A472 🌴 SPT PhenomenologyV. Kulygin

A908 Performance Assessment of a Micro- Gridded Ion Thruster DesignP. Harte

A442 Integration and Function-al Test Results of Xenon Feed Unit for Electric Propulsion SubsystemY. Yurttas

A138 Status Update on the Electric Propulsion Subsystem of TURKSAT6A Communication SatelliteB. C. Aydin

A258 Thrust measurements using plasma pressure measurements in the plume: a feasibility studyP.-Q. Elias

10.0

0

A479 🌴 Predicting secondary electron emission rate in Hall Effect ThrustersA. Tavant

A541 A Novel Miniature Xenon Feeding Module for Hall Electric ThrusterC. Guan

A923 Final Operations of the Dawn Ion Propulsion System andthe Success-ful Conclusion of the Dawn MissionC. E. Garner

A887 Recent Advances in Plasma Diagnostics at IRSG. Herdrich

10.1

5

A514 🌴 Enhancing thrust by ion-neutral collisions and by oscillating EM fieldsA. Fruchtman

A891 Towards a Microfluidic Flow Control Unit for HEMP ThrustersJ. Haderspeck

A429 The Comet Astrobiology Exploration Sample Return (CAESAR) MissionM. Sekerak

A345 Development of a Flight Electric Propulsion Diagnostic Package (EPDP) for EP Satellite PlatformsT. Trottenberg

10.3

0

A523 🌴 Effects of large scale structures on anomalous transport in PIC simula-tions of Electron Cyclotron Drift Instability in Hall thrustersA. Smolyakov

A917 Qualification Program of a Composite Overwrapped Xenon Propellant Tank for a GEO Satellite MissionS. Ontaç

A927 Mars Sample Return - Earth Return Orbiter: ESAs next Interplanetary Electric Propulsion Mission ConceptO. Sutherland

←

Friday

Documents

IEPC Programm Master 2 · mover permanent magnets for changing a magnetic field Y. Takao A835 Computer Modeling of Non-Emission Electron Source with High Frequency Ionization S. Roshanpour