RITs and more, EP activities at Giessen
|
|
- Annice Pearson
- 6 years ago
- Views:
Transcription
1 RITs and more, EP activities at Giessen Peter J. Klar, I. Physikalisches Institut, Justus-Liebig-University of Giessen, Germany
2 Topics that we are interested in Competitiveness of the European Space Sector: Technology and Science COMPET Technologies for European non-dependence and competitiveness COMPET SRC In-Space electrical propulsion and station keeping COMPET Scientific instrumentation COMPET Technologies for European non-dependence and competitiveness COMPET Competitiveness in Earth observation mission technologies COMPET Space Portal Any cooperation related to EP: thruster design, development, diagnostics, testing, material issues electronics 2 Folie 2 NKS Raumfahrt, Dr. Adrian klein
3 Heritage 1963 Invention of the RIT-concept by Prof. Löb (RIT: Radio-frequency ion-thruster) Since 1970 commercialization of RIT- 10 and other RITs towards flight hardware by (now) Airbus DS 1992, 2001 first space flights We represent Giessen - home of the RITs.
4 Inter-institutional Research Laboratory for EP Engineering Physics, Chemistry Materials Sciences We are the largest research cluster working on EP in Germany. DLR Gö Cooperation agreement Airbus DS Cooperation agreement
5 Interinstitutional Research Lab research fields Elec. eng. based modelling Ricklefs Microscopic modelling Henrich, Heiliger Complex plasma ISS-experiments Thoma, Kretschmer EMV Thüringer planned professorship space electronics Elektronics development Probst, Frey Ion thruster technology Leiter (honorary professorship) RIT-technology Test facillities Holste, Klar, Hannemann Miniaturised EP Henning, Klar, Janek Plasmadiagnostics Schippers, Mitić, Brinkmann SC/EP interaction Hannemann, Klar Alternative propellants Klar, Schreiner Our interdisciplinary team consists of about 10 research groups of different expertise.
6 EMC / EMI Baruth, Thueringer Numerical modeling Volkmar, Ricklefs Control engineering / development of peripheral devices Simon, Wolf, Probst We know how to develop electronics for EP. Ubbo Ricklefs et al. Slide
7 Test facilities at U. Giessen We provide large EP test facilities. Jumbo ipott BigMac
8 Research highlight: Diagnostics development We perform diagnostics inside thrusters and of the plume. Methods Faraday cups Retarding potential analyzers Emittance measurements Laser spectroscopy Mass spectrometry Langmuir probes
9 Research highlight: Microscopic modelling PlasmaPIC a 3D plasma simulation tool, also for rf-plasma! plasma and neutral gas simulation combined (PIC / DSMC) Parallel computing 800 cores We simulate plasma and plume of thrusters ab initio ion density in m -3
10 Research highlight: Miniaturized colloid emitters We work on miniaturized EP concepts.
11 Research highlight: Alternative propellants We work on material issues such as alternative EP propellants. 0, RIT-10 operating with C 10 H 16 Ion current [na] 0,0015 0,0010 0,0005 0,0000 reference peak: Argon RIT-10 5sscm-Ar, 1.0 sccm-c 10 H 16 (relativ to N 2 )) Adamantane RF-power [W] ma Xenon 7.5 ma Adamantan 10 ma Xenon 10 ma Adamantan RIT Mass-to-charge ratio [amu/q] 0,1 0,2 0,3 0,4 0,5 0,6 0,7 Mass-flow [sccm]
12 Summary Research cluster of two universities Expertise in EP covering thruster design, development, diagnostics, testing, material issues, electronics We hold several ESA and DLR grants, projects with industry, e.g. Airbus DS We are interested in cooperating with project partners who need our expertise in EP. 12 Folie 12 NKS Raumfahrt, Dr. Adrian klein
Self-consistent Simulation of the Coupling Between Plasma and Neutral Gas in µn-rit
Self-consistent Simulation of the Coupling Between Plasma and Neutral Gas in µn-rit IEPC-2011-323 Presented at the 32 nd International Electric Propulsion Conference, Wiesbaden, Germany R. Henrich, D.
More informationCharacterization of the operation of RITs with iodine
Characterization of the operation of RITs with iodine IEPC-2017-368 Presented at the 35th International Electric Propulsion Conference Georgia Institute of Technology Atlanta, Georgia USA Waldemar Gärtner
More informationThe µnrit-4 Ion Engine: a first step towards a European mini-ion Engine System development.
The µnrit-4 Ion Engine: a first step towards a European mini-ion Engine System development. IEPC-2007-218 Presented at the 30 th International Electric Propulsion Conference, Florence, Italy D. Feili*
More informationNew 2d Far Field Beam Scanning Device at DLR s Electric Propulsion Test Facility
New 2d Far Field Beam Scanning Device at DLR s Electric Propulsion Test Facility IEPC-2015-b/IEPC-388 Presented at Joint Conference of 30th International Symposium on Space Technology and Science 34th
More informationBeam Diagnostics for Mini Ion Engines
Beam Diagnostics for Mini Ion Engines IEPC-2013-297 Presented at the 33 rd International Electric Propulsion Conference, The George Washington University, Washington, D.C., USA Peter E. Köhler and Bruno
More informationAvailable online at ScienceDirect. Procedia Engineering 185 (2017 ) Andreas Neumann a,*
Available online at www.sciencedirect.com ScienceDirect Procedia Engineering 185 (2017 ) 47 52 6 th Russian-German Conference on Electric Propulsion and Their Application Update on diagnostics for DLR
More informationIn-situ temperature, grid curvature, erosion, beam and plasma characterization of a gridded ion thruster RIT-22
In-situ temperature, grid curvature, erosion, beam and plasma characterization of a gridded ion thruster RIT-22 IEPC-2009-160 Presented at the 31st International Electric Propulsion Conference, University
More informationIon Acceleration Modes in a Miniature Helicon Thruster
Ion Acceleration Modes in a Miniature Helicon Thruster Timothy A. Collard, Frans H. Ebersohn, J. P. Sheehan, and Alec D. Gallimore Friday, October 16, 2015 Honolulu, HI CubeSat Affordable Platform, Limited
More informationComputer modeling and comparison with diagnostic results of a downscaled High Efficiency Multi Stage Plasma Thruster
www.dlr.de Chart 1 Computer modeling and comparison with diagnostic results of a downscaled High Efficiency Multi Stage Plasma Thruster T. Brandt 1,3+, Th. Trottenberg 3, R. Groll 2, F. Jansen 1, Fr. Hey
More informationXXIV. Erfahrungsaustausch Oberflächentechnologie mit Plasma- und Ionenstrahlprozessen. Mühlleithen / Vogtland
UNIVERSITY OF APPLIED SCIENCES XXIV. Erfahrungsaustausch Oberflächentechnologie mit Plasma- und Ionenstrahlprozessen Mühlleithen / Vogtland Status Report: Numerical 3D Ion Extraction Code incorporated
More informationDevelopment of a capacitively coupled insert-free RF-neutralizer
Development of a capacitively coupled insert-free RF-neutralizer IEPC-2005-086 Presented at the 29 th International Electric Propulsion Conference, Princeton University, St. Weis, K. - H. Schartner, H.
More informationµnrit A New Optimized Microthruster Of Giessen University IEPC
µnrit-2.5 - A New Optimized Microthruster Of Giessen University IEPC-2009-174 D. Feili 1, B. Lotz, St. Bonnet, B. K. Meyer, H.W. Loeb Justus Liebig University Giessen, Heinrich-Buff-Ring 16, 35392 Giessen
More informationExperimental Validation of RIT Micro-Propulsion Subsystem Performance at EPL
Experimental Validation of RIT Micro-Propulsion Subsystem Performance at EPL IEPC-2013-90 Presented at the 33rd International Electric Propulsion Conference, Washington DC, USA, D. Di Cara 1, A. Bulit
More informationDevelopment of a Micro- Thruster Test Facility which fulfils the LISA requirements
Development of a Micro- Thruster Test Facility which fulfils the LISA requirements Franz Georg Hey 1,2, A. Keller 1, J. Ulrich 1, C. Braxmaier 3,4, M. Tajmar 2, E. Fitzsimons 1, and D. Weise 1 1 Airbus
More informationCommissioning of the Aerospazio s vacuum facilities with Safran s Hall Effect Thruster
Commissioning of the Aerospazio s vacuum facilities with Safran s Hall Effect Thruster IEPC-2017-414 Presented at the 35th International Electric Propulsion Conference Georgia Institute of Technology Atlanta,
More informationFigure 1, Schematic Illustrating the Physics of Operation of a Single-Stage Hall 4
A Proposal to Develop a Double-Stage Hall Thruster for Increased Efficiencies at Low Specific-Impulses Peter Y. Peterson Plasmadynamics and Electric Propulsion Laboratory (PEPL) Aerospace Engineering The
More informationMitigation of Detrimental Electric Thruster Force Measurement Effects
Mitigation of Detrimental Electric Thruster Force Measurement Effects IEPC-2017-162 Presented at the 35th International Electric Propulsion Conference Georgia Institute of Technology Atlanta, Georgia USA
More informationParametric Study of HEMP-Thruster, Downscaling to µn Thrust Levels
Parametric Study of HEMP-Thruster, Downscaling to µn Thrust Levels IEPC-2013-269 Presented at the 33 rd International Electric Propulsion Conference, The George Washington University, Washington, D.C.,
More informationPlasma Thruster Plume Simulation: Effect of the Plasma Quasi Neutrality Hypothesis
CENTROSPAZIO Plasma Thruster Plume Simulation: Effect of the Plasma Quasi Neutrality Hypothesis A. Passaro*, L.Biagioni*, and A.Vicini** * Centrospazio-CPR 56121 Pisa, Italy ** Alta S.p.A. 56121 Pisa,
More informationThrust Balance Characterization of a 200W Quad Confinement Thruster for High Thrust Regimes
Thrust Balance Characterization of a 200W Quad Confinement Thruster for High Thrust Regimes IEPC-2013-155 Presented at the 33rd International Electric Propulsion Conference, The George Washington University
More informationNeutral Pressure Measurement in an Ion Thruster Discharge Chamber
Neutral Pressure Measurement in an Ion Thruster Discharge Chamber IEPC-2013-106 Presented at the 33rd International Electric Propulsion Conference, The George Washington University Washington, D.C. USA
More informationINTERSTELLAR PRECURSOR MISSIONS USING ADVANCED DUAL-STAGE ION PROPULSION SYSTEMS
INTERSTELLAR PRECURSOR MISSIONS USING ADVANCED DUAL-STAGE ION PROPULSION SYSTEMS David G Fearn, 23 Bowenhurst Road, Church Crookham, Fleet, Hants, GU52 6HS, UK dg.fearn@virgin.net Roger Walker Advanced
More informationTesting and Comprehensive Modeling of a GIE Utilizing Atmospheric Propellants IEPC
Testing and Comprehensive Modeling of a GIE Utilizing Atmospheric Propellants IEPC-2013-354 Presented at the 33rd International Electric Propulsion Conference, The George Washington University Washington,
More informationLISA Pathfinder measuring pico-meters and femto-newtons in space
LISA Pathfinder measuring pico-meters and femto-newtons in space M Hewitson for the LPF team Barcelona, February 15th 2012 Observing from Space 2 Observing from Space 2 Observing from Space Push down to
More informationMINOTOR H2020 project for ECR thruster development
MINOTOR H2020 project for ECR thruster development D. Packan, P.Q. Elias, J. Jarrige, T. Vialis, S Correyero, S. Peterschmitt, ONERA M. Merino, A. Sánchez-Villar, E. Ahedo UNIVERSIDAD CARLOS III DE MADRID
More informationEPIC Draft ROADMAP Incremental line
EPIC Draft ROADMAP Incremental line PSA Consortium Workshop Stockholm 11/02/2015. Call 2016 COMMISSION PROCESS OPEN TECHNOLOGY-BASED SYSTEMS HALL EFFECT THRUSTER (HET) GRIDDED ION ENGINE (GIE) HEMP THRUSTER
More informationMeasurements of plasma parameters in the plume of electric propulsion devices Recent works performed at the ESA Propulsion Laboratory
Measurements of plasma parameters in the plume of electric propulsion devices Recent works performed at the ESA Propulsion Laboratory IEPC-2015-90161 Presented at Joint Conference of 30th International
More informationLow Cost Helicon Propulsion System for CubeSat future mission scenarios. T4i - University of Padova D.Pavarin
Low Cost Helicon Propulsion System for CubeSat future mission scenarios T4i - University of Padova D.Pavarin Centro di Ateneo Studi e Attività Spaziali University of Padova Padova, Italy Technology for
More informationProgress in Testing of QM and FM HEMP Thruster Modules
Progress in Testing of QM and FM HEMP Thruster Modules IEPC-2013-274 Presented at the 33rd International Electric Propulsion Conference, The George Washington University Washington, D.C. USA A. Lazurenko
More informationLawrence Berkeley National Laboratory Lawrence Berkeley National Laboratory
Lawrence Berkeley National Laboratory Lawrence Berkeley National Laboratory Title High current density beamlets from RF Argon source for heavy ion fusion applications Permalink https://escholarship.org/uc/item/6zh6c50m
More informationPerformance mapping of new gn-rits at Giessen
Performance mapping of new gn-rts at Giessen EPC-2005-252 Presented at the 29 th nternational Electric Propulsion ConJerence, Princeton University, D. Feili*,H. W. Loeb, K. H. Schartner, St. Weis, D. Kirmse,
More informationUpgraded Program of Russian Lunar Landers: Studying of Lunar Poles
Upgraded Program of Russian Lunar Landers: Studying of Lunar Poles I.G.Mitrofanov, L.M.Zelenyi and V.I.Tret yakov Institute for Space Research, Moscow, Russia Slide - 1 Main Goals of the Program: 1. To
More informationEffect of Plasma Plume on CubeSat Structures as a Function of Thrust Vectoring
Effect of Plasma Plume on CubeSat Structures as a Function of Thrust Vectoring IEPC-2015-157 /ISTS-2015-b-157 Presented at Joint Conference of 30th International Symposium on Space Technology and Science
More informationDownscaling a HEMPT to micro-newton Thrust levels: current status and latest results
Downscaling a HEMPT to micro-newton Thrust levels: current status and latest results IEPC-2015-377/ISTS-2015-b-377 Presented at Joint Conference of 30th International Symposium on Space Technology and
More informationAn Interferometric Force Probe for Thruster Plume Diagnostics
An Interferometric Force Probe for Thruster Plume Diagnostics IEPC-2015-419/ISTS-2015-b-419 Presented at Joint Conference of 30th International Symposium on Space Technology and Science, 34th International
More informationModular Low Earth Orbital-Hub DLR Vision 2025
The Space Congress Proceedings 2016 (44th) The Journey: Further Exploration for Universal Opportunities May 25th, 10:45 AM Modular Low Earth Orbital-Hub DLR Vision 2025 Dr. Oliver Romberg German Space
More informationImprovement of Propulsion Performance by Gas Injection and External Magnetic Field in Electrodeless Plasma Thrusters
Improvement of Propulsion Performance by Gas Injection and External Magnetic Field in Electrodeless Plasma Thrusters IEPC-217-249 Presented at the th International Electric Propulsion Conference Georgia
More informationAbstract. Objectives. Theory
A Proposal to Develop a Two-Stage Gridless Ion Thruster with Closed Electron Drift Richard R. Hofer Plasmadynamics and Electric Propulsion Laboratory (PEPL) Department of Aerospace Engineering University
More informationPrototyping and Optimization of a Miniature Microwave- Frequency Ion Thruster
Prototyping and Optimization of a Miniature Microwave- Frequency Ion Thruster IEPC-2017-516 Presented at the 35th International Electric Propulsion Conference Georgia Institute of Technology Atlanta, Georgia
More informationElectric Propulsion Propellant Flow within Vacuum Chamber
Electric Propulsion Propellant Flow within Vacuum Chamber 2015-b/IEPC-360 Presented at Joint Conference of 30th International Symposium on Space Technology and Science 34th International Electric Propulsion
More informationHelicon Plasma Thruster Persepective and At University of Padua
Helicon Plasma Thruster Persepective and Development status and future development At University of Padua D.Pavarin, M.Manente, F.Trezzolani, A.Selmo, M.Magarotto, E.Toson Outline Helicon Thruster overview
More informationHelicon Double Layer Thruster Performance Enhancement via Manipulation of Magnetic Topology
Helicon Double Layer Thruster Performance Enhancement via Manipulation of Magnetic Topology IEPC--97 Presented at the nd International Electric Propulsion Conference, Wiesbaden, Germany S. J. Pottinger,
More informationJUICE: the first European mission to Jupiter and its Icy Moons
JUICE: the first European mission to Jupiter and its Icy Moons Giuseppe Sarri Knowledge Transfer Seminar @ CERN 26 April 2018 ESA UNCLASSIFIED - For Official Use European Space Agency (ESA) The European
More informationJuly 4 10, D. Feili 1, M. Smirnova 1, M. Dobkevicius 1 University of Southampton, SO17 1BJ, Southampton, GB
Design, Construction and Testing of a Radio Frequency Mini Ion Engine According to the Propulsion Requirements of the Next Generation Gravity Missions NGGM IEPC-2015-277/ISTS-2015-b-277 Presented at Joint
More informationIEPC Presented at the 35th International Electric Propulsion Conference Georgia Institute of Technology Atlanta, Georgia USA
Highly Efficient Miniaturized Hall-Type Thruster and Rotamak Projects in Plasma Sources and Application Centre at the Nanyang Technological University, Singapore IEPC-2017-591 Presented at the 35th International
More informationHuashun Zhang. Ion Sources. With 187 Figures and 26 Tables Э SCIENCE PRESS. Springer
Huashun Zhang Ion Sources With 187 Figures and 26 Tables Э SCIENCE PRESS Springer XI Contents 1 INTRODUCTION 1 1.1 Major Applications and Requirements 1 1.2 Performances and Research Subjects 1 1.3 Historical
More informationExperimental Studies of Ion Beam Neutralization: Preliminary Results
Experimental Studies of Ion Beam Neutralization: Preliminary Results N. Ding, J. Polansky, R. Downey and J. Wang Department of Astronautical Engineering University of Southern California Los Angeles, CA
More informationThe ULAN Test Station and its Diagnostic Package for Thruster Characterization
The ULAN Test Station and its Diagnostic Package for Thruster Characterization IEPC-27-119 Presented at the 3 th International Electric Propulsion Conference, Florence, Italy Hans-Peter Harmann *, Norbert
More informationA review of plasma thruster work at the Australian National University
A review of plasma thruster work at the Australian National University IEPC-2015-90850 Presented at Joint Conference of 30th International Symposium on Space Technology and Science 34th International Electric
More informationPrincipal VASIMR Results and Present Objectives
Principal VASIMR Results and Present Objectives Tim W. Glover 1,2, Franklin R. Chang Diaz 1, Jared P. Squire 1,2, Verlin P. Jacobson 1,2, D. Gregory Chavers 3, and Mark D. Carter 4 1 NASA Advanced Space
More informationReal-time in situ determination of inductively coupled power and numerical prediction of power distribution in RF ion thrusters
Real-time in situ determination of inductively coupled power and numerical prediction of power distribution in RF ion thrusters IEPC-2017-161 Presented at the 35th International Electric Propulsion Conference
More informationThe Quad Confinement Thruster - Preliminary Performance Characterization and Thrust Vector Control
The Quad Confinement Thruster - Preliminary Performance Characterization and Thrust Vector Control IEPC-2011-099 Presented at the 32 nd International Electric Propulsion Conference, Wiesbaden, Germany
More informationDevelopment and Test of XR-150, a New High-Thrust 100 W Resistojet
Development and Test of XR-150, a New High-Thrust 100 W Resistojet IEPC-2013-219 Presented at the 33rd International Electric Propulsion Conference, The George Washington University Washington, D.C. USA
More informationComprehensive Radio Frequency Ion Thruster Electromagnetic and Thermal Modelling
Comprehensive Radio Frequency Ion Thruster Electromagnetic and Thermal Modelling IEPC-2015-410/ISTS-2015-b-410 Presented at Joint Conference of 30th International Symposium on Space Technology and Science
More informationComputational Modeling of a High Power Plasma Source for Material Interaction Experiments
Computational Modeling of a High Power Plasma Source for Material Interaction Experiments IEPC-2013-224 Presented at the 33rd International Electric Propulsion Conference, The George Washington University
More informationPropulsion means for CubeSats
Propulsion means for CubeSats C. Scharlemann and D. Krejci 2009 CubeSat Developers Workshop, San Louis Obispo, CA Welcome to the Austrian Research Centers Space Propulsion & Advanced Concepts Staff: 11
More informationInitial performance characterisation of a plasma thruster employing magnetic null regions
Initial performance characterisation of a plasma thruster employing magnetic null regions IEPC-215-45/ISTS-215-b-45 Presented at Joint Conference of 3th International Symposium on Space Technology and
More informationMEASUREMENT OF THE ION DRAG FORCE IN A COMPLEX DC- PLASMA USING THE PK-4 EXPERIMENT
MEASUREMENT OF THE ION DRAG FORCE IN A COMPLEX DC- PLASMA USING THE PK-4 EXPERIMENT M.H.THOMA 1, H. HÖFNER 1, S. A. KHRAPAK 1, M. KRETSCHMER 1, R.A. QUINN 1, S. RATYNSKAIA 1, G.E. MORFILL 1, A. USACHEV,
More informationAlex Samarian School of Physics, University of Sydney, NSW 2006, Australia
Alex Samarian School of Physics, University of Sydney, NSW 2006, Australia What is Dusty (Complex) Plasma? Laboratory Dusty Plasma Why Study Complex (Dusty) Plasma? Worldwide Research Activities Complex
More informationCharacterization of an adjustable magnetic field, low-power Hall Effect Thruster
Characterization of an adjustable magnetic field, low-power Hall Effect Thruster IEPC-2011-143 Presented at the 32nd International Electric Propulsion Conference, Wiesbaden Germany S. Oslyak 1, C. Ducci
More informationTHE DLR ORBITAL HUB: A CONCURRENT ENGINEERED POST-ISS APPROACH
THE DLR ORBITAL HUB: A CONCURRENT ENGINEERED POST-ISS APPROACH www.dlr.de Folie 2 > Orbital-Hub > O. Romberg, Oct 2016 THE DLR ORBITAL HUB: A CONCURRENT ENGINEERED POST-ISS APPROACH 7th International Conference
More informationMicro Electric Propulsion Technology for Small Satellites: Design, Testing and In-Orbit Operations
SSC13-III-9 Micro Electric Propulsion Technology for Small Satellites: Design, Testing and In-Orbit Operations V.J. Lappas, T. Harle, A. Knoll, P. Shaw University of Surrey, Guildford, GU2 7XH P. Bianco
More informationILWS activity in Romania
Institute of Space Science romanian space agency ILWS activity in Romania Dumitru HASEGAN 1,2. Octav MARGHITU 1 1-ISS, 2-ROSA Outline A. Introduction Historical synopsis B. Research themes 1. Solar-Terrestrial
More informationPico-Satellite Orbit Control by Vacuum Arc Thrusters as Enabling Technology for Formations of Small Satellites
1/25 Pico-Satellite Orbit Control by Vacuum Arc Thrusters as Enabling Technology for Formations of Small Satellites Igal Kronhaus, Mathias Pietzka, Klaus Schilling, Jochen Schein Department of Computer
More informationParticle Simulation of Hall Thruster Plumes in the 12V Vacuum Chamber
Particle Simulation of Hall Thruster Plumes in the 12V Vacuum Chamber IEPC-2005-138 Presented at the 29 th International Electric Propulsion Conference, Princeton University, Iain D. Boyd 1, Quanhua Sun
More informationSolar & Electric Sailing Overview
Solar & Electric Sailing Overview KISS Technology Development Workshop (May 15-18, 2018) NASA Image NASA Image Jared Dervan NASA/MSFC Acknowledgments Les Johnson (MSFC Project Formulation Office) Bruce
More informationOverview, Qualification and Delivery Status of the HEMP- Thruster based Ion Propulsion System for SmallGEO
Overview, Qualification and Delivery Status of the HEMP- Thruster based Ion Propulsion System for SmallGEO IEPC-2017-197 Presented at the 35th International Electric Propulsion Conference, Georgia Institute
More informationA Hours Endurance Testing of RIT-22 Thruster in the New Aerospazio Test Facility
A.000 Hours Endurance Testing of RIT- Thruster in the New Aerospazio Test Facility IEPC-005- Presented at the 9 th International Electric Propulsion Conference, Princeton University, E. Bonelli *, S. Scaranzin
More informationSystem and Concurrent Engineering for the e.deorbit Mission Assessment Studies Robin Biesbroek Jakob Hüsing Andrew Wolahan
System and Concurrent Engineering for the e.deorbit Mission Assessment Studies Robin Biesbroek Jakob Hüsing Andrew Wolahan Why Active Debris Removal? 17000 catalogued objects Less than 1000 active 600-800
More informationThe MINOTOR H2020 project for ECR thruster development
The MINOTOR H2020 project for ECR thruster development IEPC-2017-547 Presented at the 35th International Electric Propulsion Conference Georgia Institute of Technology Atlanta, Georgia USA D. Packan 1,
More informationNumerical procedure permitting calculation of how a vacuum chamber influences Electric Propulsion Thruster jet expansion.
Numerical procedure permitting calculation of how a vacuum chamber influences Electric Propulsion Thruster jet expansion. 2X-H0H1A6G7B1 Presented at the 30th International Electric Propulsion Conference,
More informationExperimental Analysis of a Low-Power Helicon Thruster
Experimental Analysis of a Low-Power Helicon Thruster Douglas Palmer, Mitchell L. R. Walker High-Power Electric Propulsion Laboratory Georgia Institute of Technology, Atlanta, GA, USA M. Manente, D. Pavarin
More informationVery High I sp Thruster with Anode Layer (VHITAL): An Overview
Space 2004 Conference and Exhibit 28-30 September 2004, San Diego, California AIAA 2004-5910 Very High I sp Thruster with Anode Layer (VHITAL): An Overview Colleen M. Marrese-Reading * Robert Frisbee Anita
More informationDevelopment of stationary plasma thruster SPT-230 with discharge power of kw
Development of stationary plasma thruster SPT-230 with discharge power of 10...15 kw IEPC-2017-548 Presented at the 35th International Electric Propulsion Conference Georgia Institute of Technology Atlanta,
More informationElectric Propulsion Activities at ONERA
Electric Propulsion Activities at ONERA IEPC-2015-92094 Presented at Joint Conference of 30th International Symposium on Space Technology and Science 34th International Electric Propulsion Conference and
More informationInitial Experiments of a New Permanent Magnet Helicon Thruster
Initial Experiments of a New Permanent Magnet Helicon Thruster J. P. Sheehan 1, B. W. Longmier 1, I. M. Reese 2, T. A. Collard 1, F. H. Ebersohn 1, E. T. Dale 1, B. N. Wachs 1, and M. E. Ostermann 1 1
More informationEffects of the Gas Pressure on Low Frequency Oscillations in E B Discharges
Effects of the Gas Pressure on Low Frequency Oscillations in E B Discharges IEPC-2015-307 /ISTS-2015-b-307 Presented at Joint Conference of 30th International Symposium on Space Technology and Science
More informationLaser Ablation Studies at UCSD and Plans for Time and Space Resolved Ejecta Measurements
Laser Ablation Studies at UCSD and Plans for Time and Space Resolved Ejecta Measurements M. S. Tillack, Y. Tao, Y. Ueno*, R. Burdt, S. Yuspeh, A. Farkas, 2 nd TITAN workshop on MFE/IFE common research
More informationElectric Propulsion. An short introduction to plasma and ion spacecraft propulsion. S. Barral. Instytut Podstawowych Problemów Techniki - PAN
Electric Propulsion An short introduction to plasma and ion spacecraft propulsion S. Barral Instytut Podstawowych Problemów Techniki - PAN sbarral@ippt.gov.pl S. Barral (IPPT-PAN) Electric Propulsion 1
More informationBRINGING YOUR EXPERIMENT INTO SPACE
BRINGING YOUR EXPERIMENT INTO SPACE Science Service Division SSC - Swedish Space Corporation Space exploration with ESA: opportunities within the ESA programme E3P Stockholm, 13 November 2018 SWEDISH SPACE
More informationExperimental Investigations of Magnetoplasmadynamic Thrusters with Coaxial Applied Magnetic Field IEPC
Experimental Investigations of Magnetoplasmadynamic Thrusters with Coaxial Applied Magnetic Field IEPC-2007-141 Presented at the 30 th International Electric Propulsion Conference, Florence, Italy Daniel
More informationSpatial Profile of Ion Velocity Distribution Function in Helicon High-Density Plasma by Laser Induced Fluorescence Method
Trans. JSASS Aerospace Tech. Japan Vol. 14, No. ists3, pp. Pb_7-Pb_12, 216 Spatial Profile of Ion Velocity Distribution Function in Helicon High-Density Plasma by Laser Induced Fluorescence Method By Yuriko
More informationNumber Density Measurement of Xe I in the ECR Ion Thruster µ10 Using Optical Fiber Probe
Number Density Measurement of Xe I in the ECR Ion Thruster µ10 Using Optical Fiber Probe IEPC-2011-318 Presented at the 32nd International Electric Propulsion Conference, Wiesbaden Germany Ryudo Tsukizaki
More informationCold Gas Thruster Qualification for FORMOSAT 5
Cold Gas Thruster Qualification for FORMOSAT 5 By Hans-Peter HARMANN 1), Tammo ROMBACH 2) and Heiko DARTSCH 1) 1) AST Advanced Space Technologies GmbH, Stuhr, Germany 2) SpaceTech GmbH, Immenstaad, Germany
More informationAlberto Garbayo - MEng (hons) CEng Business Development Manager
www.a-v-s.uk.com SME Engineering company with headquarters near Bilbao, Spain and Harwell Campus, Oxfordshire, UK. Founded in 2006, formed by highly qualified personnel (80% MEng, MSc and Doctors) with
More informationNumerical Studies of Micro-Cathode Arc Thruster Plume Expansion
Numerical Studies of Micro-Cathode Arc Thruster Plume Expansion IEPC-2015-57/ISTS-2015-b-57 Presented at Joint Conference of 30th International Symposium on Space Technology and Science, 34th International
More informationCalibration of Particle Instruments in Space Physics
SR-007 September 2007 Calibration of Particle Instruments in Space Physics Editors Martin Wüest INFICON Ltd, Balzers, Principality of Liechtenstein David S. Evans Space Environment Center, NOAA, Boulder
More informationDevelopment of Microwave Engine
Development of Microwave Engine IEPC-01-224 Shin SATORI*, Hiroyuki OKAMOTO**, Ted Mitsuteru SUGIKI**, Yoshinori AOKI #, Atsushi NAGATA #, Yasumasa ITO** and Takayoshi KIZAKI # * Hokkaido Institute of Technology
More informationEndurance Testing of HEMPT-based Ion Propulsion Modules for SmallGEO
Endurance Testing of HEMPT-based Ion Propulsion Modules for SmallGEO IEPC-211-141 Presented at the 32nd International Electric Propulsion Conference, Wiesbaden Germany A. Genovese, 1 A. Lazurenko, 2 N.
More informationDEVELOPMENT AND PERFORMANCE OF THE ADVANCED RADIO FREQUENCY ION THRUSTER RIT-XT
DEVELOPMENT AND PERFORMANCE OF THE ADVANCED RADIO FREQUENCY ION THRUSTER RIT-XT Hans.J.Leiter, Rainer Killinger, Helmut Bassner, Johann Müller, Ralf Kukies, Thomas Fröhlich Astrium GmbH Space Infrastructure
More informationTAU Extensions for High Enthalpy Flows. Sebastian Karl AS-RF
TAU Extensions for High Enthalpy Flows Sebastian Karl AS-RF Contents Motivation Extensions available in the current release: Numerical schemes for super- and hypersonic flow fields Models for gas mixtures,
More informationPlasma Spectroscopy CubeSat: A demonstration of on-orbit electric propulsion system diagnostics
Plasma Spectroscopy CubeSat: A demonstration of on-orbit electric propulsion system diagnostics Jennifer Hudson and Kristina Lemmer Department of Mechanical and Aerospace Engineering, Western Michigan
More informationNon-Phase-Difference Rogowski Coil for Measuring Pulsed Plasma Thruster Discharge Current
Non-Phase-Difference Rogowski Coil for Measuring Pulsed Plasma Thruster Discharge Current IEPC-2015-49/ISTS-2015-b-49 Presented at Joint Conference of 30th International Symposium on Space Technology and
More informationProfessor Alec Gallimore Department of Aerospace Engineering University of Michigan. 11 October 2013
Professor Alec Gallimore Department of Aerospace Engineering University of Michigan 11 October 2013 US Academic Programs Engaged in EP Research 30 Institutions, 40 Professors, >100 Graduate Students DoD
More informationJames Carpenter, Lunar Lander Office, Directorate of Human Spaceflight and Operations
The European Lunar Lander James Carpenter, Lunar Lander Office, Directorate of Human Spaceflight and Operations 1 International Context Apollo/Luna Era 1990-2006 2007-2012 2013-2020 Next Decade HITEN CLEMENTINE
More informationElectric Propulsion Research and Development at NASA-MSFC
Electric Propulsion Research and Development at NASA-MSFC November 2014 Early NEP concept for JIMO mission Dr. Kurt Polzin (kurt.a.polzin@nasa.gov) Propulsion Research and Development Laboratory NASA -
More information, (2) German Aerospace Center (DLR), Porz-Wahnheide, Linder Hoehe, Koeln Germany,
TRAJECTORY AND SYSTEM DESIGN OF AN ELECTRICALLY PROPELLED ORBITER FOR A MARS SAMPLE RETURN MISSION Uwe Derz (1), Wolfgang Seboldt (2) (1) EADS Astrium Space Transportation, Airbus Allee 1, 28199 Bremen
More informationInvestigation of a 5 kw class Hall-effect thruster operating with different xenon-krypton mixtures
Investigation of a 5 kw class Hall-effect thruster operating with different xenon-krypton mixtures IEPC-2015-126 /ISTS-2015-b-126 Presented at Joint Conference of 30th International Symposium on Space
More informationMeasurement of the Momentum Flux in an Ion Beam
Measurement of the Momentum Flux in an Ion Beam IEPC-2011-232 Presented at the 32 nd International Electric Propulsion Conference, Wiesbaden Germany Alexander Spethmann 1, Thomas Trottenberg 2, and Holger
More informationTwo-Dimensional Particle-in-Cell Simulation of a Micro RF Ion Thruster
Two-Dimensional Particle-in-Cell Simulation of a Micro RF Ion Thruster IEPC--7 Presented at the nd International Electric Propulsion Conference, Wiesbaden Germany September 5, Yoshinori Takao, Koji Eriguchi,
More information