Programme Content

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Programme Content

IEPC2019 wants to thank all sponsors for their support

Overview 05

Platin Monday 32

Gold Tuesday 42

Wednesday 46

Exhibitors

Thursday 54

Friday 64 Promotion Agency Supported by 2 IEPC19 Programme Welcome Note 3

The IEPC is the premier international forum for spacecraft primes, hardware developers, Overview government researchers, academic scholars, and students in the field of electric propulsion. Welcome to the Era of The programme contains more than 500 technical presentations which cover propulsion Electric Propulsion device physics and development to on-orbit operation and satellite fleet management. In space, everything is The 2019 IEPC has a rich and diverse technical moving fast. programme featuring the latest developments and research results in the field, as well as a number of informative and educational events along with technical visits to nearby facilities. Any object floating around the earth travels at least 7 kilome- ters per second. So naturally, mastering in-space mobility is key to the success of every space endeavor, be it the installation of space-based infrastructure for the benefit of earth or the exploration of our solar system. The possibility to move one’s Dr. Alexander Reissner assets from one place to another, deploy constellations, remove General Chair of IEPC 2019 dysfunctional elements and avoid collisions, autonomously and Contact on short notice, is an enabling factor in unlocking the vast potential space has to offer. I believe that the rapid developments Dr. Alexander Reissner of space-infrastructure we see today are just the beginning of General Chair a thriving near-earth economy, enabled by effective in-space ENPULSION Technical Committee mobility solutions. → [email protected] Carsten Scharlemann Today, we are entering an era in which electric propulsion is be- Käthe Dannenmayer coming the dominant choice for such in-space mobility across Michael Keidar all applications and it is up to us to define how this era will Dr. Carsten Scharlemann Paulo Lozano look. Will we be able to protect economic interests in a world of Chair of Technical Committee Stéphane Mazouffre commercial competition, without sacrificing an open exchange Fachhochschule Wiener Neustadt GmbH Rostislav Spektor about technological advancements? Will we be able to com- → [email protected] Martin Tajmar bine the best of both scientific excellence and industrial capabilities and create robust business models without sacrificing Local & Organizing Committee the academic freedom to explore new frontiers?

Katrin Fangl Alexander Reissner I believe we will, because in the last 25 years, with the careful Chair of Organizing Committee Carsten Scharlemann guidance of the ERPS, our community has grown into a global FOTEC Forschungs- und Katrin Fangl family that is based on respect and trust for each other. I believe Technologietransfer GmbH Marcella Sigmund that this community can handle competition without losing this → [email protected] Bogumila Amcha trust and respect and that it can play a defining role in the new Gerry Schneider space era without losing its identity. Nikolaus Ortner In a time when everything is moving at breakneck speed, it is Marcella Sigmund Design our communities and relationships that matter more than ever, Organisation Aerospace Engineering and it is up to us, here at the IEPC 2019, to strengthen these re- University of Applied Sciences Science Communications lationships. The way we define our community today will shape Fachhochschule Wiener Neustadt GmbH Mag. Bertram Schütz how the era of electric propulsion will look in the years to come. → [email protected] Matthias Nowak So let’s get to it. And enjoy! 4 IEPC19 Programme Schedule / Floorplan 5

Monday 16 Tuesday 17 Wednesday 18 Thursday 19 Friday 20

Speaker/Chair Briefing Speaker/Chair Briefing Speaker/Chair Briefing Speaker/Chair Briefing Speaker/Chair Briefing

08:00 BIG Hörsaal BIG Hörsaal BIG Hörsaal BIG Hörsaal BIG Hörsaal RAFAEL

Raised Ground Floor Overview Plenary Lecture Parallel Sessions Parallel Sessions Parallel Sessions Parallel Sessions Exhibition VACCO Welcoming / David C. Linde

09:00 Byers Memorial Lecture Exhibition Huazong University Startup Booths ENPULSION RUAG Plenary Lecture Buffet COBHAM EP as Enabler for Future FOTEC/ FHWN Busek 10.00 Science and Exploration Registration Desk Aerojet Rocketdyne Meeting Point Tubitak UZAY SITAEL Panel Discussion Conference Tour Accompanying Person Program EP in the Commercial Melk Abbey & Boat Trip Ariane Group 11.00 Space Area on the Danube River Safran Peak Technology Tour Briefing Audimax 11:30

Lunch Lunch / Snack / Lunch Arkadenhof Poster Session Arkadenhof

12.00 Arkadenhof

Lunch / Technical Visits 12:30 Poster Session with visit to a typical Arkadenhof ERPS Austrian Tavern Meeting

13.00 Audimax

Plenary Lecture 13:30 The Role of EP in LEO Parallel Sessions Plenary Lecture Coffee & Refreshments BepiColombo – Lower Level 14.00 The Mission Seminarraum 8 Sessions Seminarraum 7 Parallel Sessions Parallel Sessions Hörsaal 6 Sessions Coffee & Refreshments Coffee & Refreshments Hörsaal 5 Private Meeting Rooms 15.00 Others

Hörsaal 3 Hörsaal 2 Seminarraum 6 16.00 Seminarraum 5 Seminarraum 4 Seminarraum 3 Audimax

17.00 Seminarraum 2 Sessions / Seminarraum 1 Plenary Lectures Gala Dinner Speaker Ready Room Wardrobe Townhall 18.00

Hörsaal 1

19.00 Office

BIG Hörsaal Speaker and Session

20.00 Chair Briefing 21.00 6 IEPC19 Programme Area Map 7

is proud to support the 36th International Electric Propulsion Conference in Vienna !

We offer state-of-the-art electric propulsion solutions for small and medium satellites with our

IFM Nano and IFM Micro ranges based on the proprietary FEEP technology. Overview

OUR SOLUTIONS ARE:

SPACE-PROVEN - 25 thrusters already flying in orbit and another 65 delivered to customers (as of August 2019).

TESTED - we follow rigorous test procedures for thermal resistance, vibrati - on, and performance performed by highly qualified aerospace engineers and technicians in our modern facilities in Wiener Neustadt, Austria.

SAFE AND EASY TO HANDLE - IFM emitters use indium, a non-toxic, non-re - active and non-radioactive as propellant. As the propellant is pre-loaded and in solid state during launch, there is no need for pressurized tanks and pre- launch loading procedures.

MODULAR - our thrusters are engineered in a modularity approach, with units clustering easily together to form building blocks that can be arranged for various mission profiles

SCALABLE - we have implemented a lean manufacturing process, designed for high rate production while meeting the demands of space product assurance standards.

Legend University of Vienna Sights Entrance Underground Parking garage Bus Meeting Point

Tram Disabled parking spot Supermarket

ATM Pharmacy Bank 8 IEPC19 Programme Social Programme 9

Welcome Reception Spanish Riding School & Gala Dinner at the Registration for tours and Hofburg Vienna – Imperial Palace Vienna City Hall events is possible within

the registration process. Overview During the conference, ask at the registration desk if space is available. 1 4 6

Sunday 15th / 18:00 – 22:00 Wednesday 18th / 09:30 – 12:30 Wednesday 18th / 18:00 – 23:00 Photocredits 1 ©Universität Wien Arcarded Courtyard / University of Vienna Starting & End Point: University of Vienna Town Hall Vienna, Rathausplatz 1, 1010 2 ©WienTourismus / Christian Stemper Free for attendees Price: €45,00 Free for attendees 3 ©Niederösterreich-Werbung/Michael Liebert accompanying persons: €50,00 accompanying persons: €100,00 4 ©WienTourismus / Lois Lammerhuber The morning exercise of the Spanish Riding School offers an 5 ©WienTourismus / Christian Stemper 6 ©WienTourismus/Christian Stemper Enjoy the get together before the conference in the his- insight into the training of the riders and their Lipizzaners. The IEPC 2019 Award Ceremony in the ambiance of Vienna 7 © WienTourismus / Peter Rigaud toric surroundings of the University’s Arkadenhof/Arcaded The morning exercise includes relaxation exercises, the re- City Hall’s breath-taking ballroom as well as an impressive Courtyard. (If the weather is rainy and unpleasant, then the fining and perfecting of lessons and the targeted strength- dance performance will guarantee an unforgettable evening reception will be in the Main Ceremoinial Chamber). ening of muscles. The Imperial Palace was the residence of in the heart of the city. the Habsburgs for over 600 years and thus the centre of the Holy Roman Empire. Apart from its function as the seat of government and administrative centre, the “Vienna Hof- burg” was also the winter residence of the imperial family.

City Walk & St. Stephen's Cathedral Conference Tour to Melk Vienna Bus Tour: City sites, Technical Visits to Technopol Abbey with Dinner Cruise Schönbrunn Palace & Giant Wiener Neustadt and visit on the Danube River Ferris Wheel (includes Lunch) at a typical Austrian Tavern

2 3 5 7

Monday 16th / 09:00 – 12:00 Tuesday 17th / 11:00 – 22:00 Thursday 19th / 09:00 – 17:00 Friday 20th / 13:00 – 21:00 Starting & End Point: University of Vienna Starting & End Point: University of Vienna Starting & End Point: University of Vienna Starting & End Point: University of Vienna Price: €35,00 Free for attendees Price: €130,00 Free of charge for all students & accompanying persons €120,00 Explore the old town of Vienna with historic buildings and Experience Vienna by bus and then explore Schönbrunn Technopol Wiener Neustadt focuses on technology and re- monuments with the occasional contrast of a few new Melk Abbey is one of the biggest and most beautiful Eu- Palace (on foot) on the “Selected Highlights Tour”. Enjoy search aiming to establish Lower Austria as an innovative buildings. Enjoy St. Stephen’s wonderful interior with all its ropean Baroque ensembles. Its splendid architecture is your lunch (beverages are not included) at the Schönbrun- high-tech location in Europe. The goal is to connect R&D fascinating architectural details. At a height of 136.4 me- famous worldwide and part of UNESCO’s world cultural her- ner Stöckl restaurant in an imperial ambiance. A tour high- institutions with high-tech companies and academic edu- tres, St. Stephen’s South Tower is an architectural master- itage. The Baroque building situated on a cliff overlooking light is the breath-taking view of the city from the Giant cation and training institutions. piece of the late Middle Ages. (This program requires good the Danube, in the Wachau region, ranks as one of Austria’s Ferris Wheel (Note: this particular stop might not be good walking shoes and the stamina to walk and stand 3 hours. It most visited art-historical sites. Enjoy the dinner cruise on for people with acrophobia). Visited companies involves many stairs as well.) the “MS Admiral Tegetthoff” on the way back to Vienna.

Trip to Melk Abbey is available only for conference attendees. Ask at the on-site registration desk if places for accompanying persons might be available. 10 IEPC19 Programme Lectures / Awards 11

Thursday 19th / 14:00 / Audimax David C. Byers Electric Propulsion as Enabler BepiColombo – Presenter Neil Wallace Memorial Lecture for Future Science and Exploration The Mission Plenary Lecture with Agencies Plenary Lecture The development and qualification of the Electric Propul- sion system (EP) for the BepiColombo mission formally commenced in 2008 with the negotiation and award of the Overview EP development contract. In real terms however it started in Monday 16th / 10:00 / Audimax 1998 with the first designs, prototyping and testing of the Moderator Carsten Scharlemann 22cm diameter T6 thruster by QinetiQ, in their new Electric Propulsion (EP) laboratory based in Farnborough, UK. Half a Representatives from NASA, ESA and JAXA will discuss how career later, BepiColombo was launched from Kourou on an electric propulsion is enabling scientific discoveries and Ariane 5 in October 2018 and the EP system successfully Monday 16th / 09:00 / Audimax exploration in the 21st century. They will present ongoing and commissioned shortly before Christmas. Now fully opera- Moderator Roger Myers planned missions using electric propulsion, as well as major tional, the system is in the first phases of its 7 year mission Presenters Frank Curran / Mike Patterson development programs in their respective parts of the world. to transfer the spacecraft to the planet Mercury. This presentation attempts to provide a non-technical insight into In memory of David C. Byers’ tremendous impact on the some of the highs and lows of the development team during application of electric propulsion, the Electric Rocket Pro- the programme, memorable moments and achievements pulsion Society has initiated the David C. Byers Memorial The Role of Electric and to serve as an introduction to the subsequent technical Lecture, or “Byers Lecture”, to be given at a plenary session Propulsion in LEO papers of the session. of each International Electric Propulsion Conference (IEPC) Panel Discussion starting in 2019. The inaugural Byers Lecture will cele- brate Dave’s life and accomplishments and will be given by a collection of presenters selected for their knowledge of Dave’s immense contributions toward the application of EP. Following an introduction by Roger Myers, Frank Curran and Mike Patterson will review Dave’s approach to overcoming the many challenges and resistance to the “new” electric Best Poster Award for 2019 conference propulsion technology through examples from Dave’s long Wednesday 18th / 13:30 / Audimax IEPC Awards career at NASA and his support of our EP community. Moderators Rafael Spears / Mitchell Walker The International Electric Propulsion Conference Best Post- Presenters Anton Olshanskii, Alexander Reissner, er Award (BPA) is an Electric Rocket Propulsion Society Albertoni Riccardo, Umair Siddiqui (ERPS)-sponsored award that will be presented at each In- ternational Electric Propulsion Conference (IEPC). The BPA The announcement of LEO satellite constellations support- is intended to recognize the best current research in the ed by significant industrial and private investors has rede- field of EP and, for this, participants will display a visual rep- Electric Propulsion in the fined the satellite communication market. The success of resentation (poster) of their research findings at the Poster Commercial Space Era many of the constellation operator financial models hinges Session to be held on Monday 16th from 12:30 to 14:00 and th Plenary Lecture with Industry on the availability of low-cost, moderate performance, Thursday 19 from 12:00 to 14:00. high-volume electric propulsion technology. Electric propulsion start-up companies with university lineage have Best Paper for 2017 appeared to meet the new demand. These start-up com- Monday 16th / 11:00 / Audimax panies, backed by impressive venture capital investments, The Best Paper Award is awarded for each conference to Moderator Alexander Reissner join a competitive electric propulsion supplier community. all co-authors of the selected paper. This Award recogniz- Long before the satellite constellations are successfully es the authors of the paper which is judged to be the best How is the rise of commercial space affecting the econom- demonstrated, constellations operators must make impor- in terms of quality, innovativeness, and significance of the ics of electric propulsion? What are the expectations of both tant decisions with respect to the ability of these compa- work described. It also recognizes excellence of the pres- satellite integrators and operators? How do Heritage Space nies to become sustainable propulsion suppliers. The goal entation. Customers and New Space Customers see the implementa- of the panel discussion is to ask the questions that will Stuhlinger Medal tion of industrial processes into electric propulsion manu- distill the necessary conditions for the long-term viability of Kuriki Award for Young Professionals facturing? What does the emergence of commercially driv- the new entrants to the electric propulsion supplier market. The Stuhlinger Medal of Outstanding Achievement in Elec- en business models mean? How do these developments fit The panel is composed of technical leaders of the new EP The “Kuriki Award for Young Professionals” (Kuriki Award) tric Propulsion is meant to be and remain the highest dis- with the needs and timelines of scientific missions? Those companies. The questions and participant selection aim to was announced to the Electric Rocket Propulsion Society tinction given by the ERPS in recognition of outstanding questions will be discussed amongst representatives from generate a healthy and meaningful debate with respect to (ERPS) community in November of 2016 and will be pre- technical or leadership contributions in Electric Propulsion all relevant stakeholders of the changing environment in the present and future role of EP for small satellites. The sented at each International Electric Propulsion Conference engineering, science, technology, education, management, which electric propulsion is already bound to play a key role panel is of interest to the EP community and space invest- (IEPC) in honor of Dr. Kyoichi Kuriki’s tremendous contribu- information exchange, or influencing programs that have led in the future. ment community because it will provide fascinating insights tions to the advancement of Electric Propulsion (EP). to important advancement in the field. into the unique dynamics of the LEO supply chain. 12 IEPC19 Programme Index A → C 13

Author and Session Chair Information Chairs in Index are marked C = Chairs start Name A → Z Monday 16 Tuesday 17 Wednesday 18 Thursday 19 Friday 20

Abrantes, R. J. 09:15 HS3 Speaker and Chair briefing Speakers practicing room Ahedo Galilea, E. 11:15 HS5 Every morning during the conference (Monday to Friday), Speakers who wish to practice their presentation may do Ahedo, E. 05:15 C HS3 09:00 HS5 Overview from 08:00 to 09:00, a speaker and chair briefing is offered so in “Seminarraum 1/Speaker Ready Room” (see floor Akhare, D. 17:00 HS2 in the “BIG Hörsaal” (see floorplan on page 5). Authors who plan on page 7). A sign-up sheet is located on the door of Akhmetzhanov, R. 15:15 HS5 are presenting on this day will meet with the chairs of their “Seminarraum 1”. Please sign up for a 30 minute-slot. In Altmann, C. 09:00 C HS5 respective session for a short session briefing. Please at- consideration to others, please limit your practice time to Andreano, T. 16:00 SR2 tend on the day of your presentation or if you are a chair on a maximum of a 30 minute increment. Andrenucci, M. 14:00 C SR3 that day. Information about the organization of the session and tasks of the chairs will be provided during this briefing. Session rooms Andreussi, T. 14:15 SR6 09:00 SR2 17:00 HS3 09:00 C HS6 Speakers are asked to provide a very short bio (name and Each session room is equipped with a computer/laptop, 17:00 SR6 10:45 SR6 affiliation) to the chairs of their session such that the chairs LCD projector, screen, microphone and sound system. The Antypas, R. 14:45 SR5 can introduce them during the session. presenters are encouraged to provide their presentation Aoyagi, J. 17:00 SR4 on a memory stick. If you choose to use your own com- Arai, Y. 15:30 HS2 Session chair report puter, please arrive well in time before a session to have Araki, S. 16:00 C SR2 09:00 SR2 All session chairs are asked to complete a session chair sufficient margin to test the compatibility of your system Arthur, N. 10:15 HS5 report. The report will be provided in each session room with the one provided in the session room. Technical as- Ataka, Y. 16:30 HS5 prior to the start of the session. More information about the sistance is provided in each session room in case you en- Aydin, B. C. 09:45 HS2 report and the general tasks of the chairs will be provided counter difficulties. Bai, S. 09:30 HS2 each morning during the “Speaker and Chair Briefing” Baird, M. 09:45 SR6 11:00 SR6 Bak, J. 10:00 SR6 Barbier, P. 09:00 C SR5 Bathgate, S. 17:15 HS2 Battista, F. 16:15 SR6 Bauer, P. 18:15 HS5 Baxter, T. 11:15 HS2 Becatti, G. 14:00 C HS6 09:45 HS6 10:45 HS6 Behnke, A. 09:00 SR3 Bello-Benítez, E. 09:15 HS6 Radiofrequency Ion Technology — RIT Berenguer, C. 18:00 HS3 Berger, M. 09:30 HS6 17:00 HS5 Blanchet, A. 10:00 HS3 › EFFICIENT with the highest Isp Blaser, M. 09:15 SR3 Boeuf, J.-P. 15:45 SR2 › VERSATILE with several function modes Boniface, C. 14:45 HS2 09:00 C SR6 › MODULAR with building blocks Bosch, E. 16:00 C HS2 09:00 C HS5 Bosi, F. 11:30 HS6 › PROVEN in space and with extensive tests 15:00 C HS6 Bourguignon, E. 10:00 SR3 Boxberger, A. 10:15 SR3 15:00 C SR3 Brieda, L. 10:00 SR2 15:00 SR4 Brophy, J. 14:00 C HS3 09:00 HS3 09:30 HS5 15:00 C HS5 Brown, N. 09:15 SR6 Brown, Z. 10:15 HS5 Byrne, M. 18:15 SR2 Cannat, F. 16:00 HS5 09:45 HS5 Cao, X.-F. 10:30 SR2 ArianeGroup’s electric space propulsion expertise is based on the space proven Radiofrequency Ion Technology (RIT). Carroll, D. 14:45 SR4 Within this field we produce complete propulsion systems, modules, thrusters and related components. For more information please contact: [email protected] Cassady, J. 14:15 SR3 09:00 C HS3 14 IEPC19 Programme Index C → E 15

Name A → Z Monday 16 Tuesday 17 Wednesday 18 Thursday 19 Friday 20 Name A → Z Monday 16 Tuesday 17 Wednesday 18 Thursday 19 Friday 20

Chan, Y.-A. 10:30 HS3 Cui, K. 09:30 SR2 17:15 HS3 Cusson, S. 15:00 SR2 Chang, L. 09:15 SR4 17:45 SR6 Overview Chaplin, V. 14:00 SR2 Dale, E. 16:30 SR2 14:15 SR2 17:00 SR2 Charoy, T. 09:00 SR2 Daniels, K. 17:15 SR4 Che, B. 16:00 C SR4 09:00 HS3 Dannenmayer, K. 09:00 C HS2 09:00 C SR4 Chen, J. 16:00 SR2 Davis, M. 17:15 SR5 Chen, K.-Y. 11:00 HS3 Daykin-Iliopoulos, A. 16:15 HS6 Chen, X. 15:30 HS6 09:00 C HS6 Degremont, J. 15:00 HS2 Chenguang, L. 09:30 HS2 Demmons, N. 14:30 SR5 Cho, S. 15:30 SR2 Dietz, C. 15:45 HS2 Choueiri, E. 10:30 HS2 Dietz, P. 09:15 HS6 Ciaralli, S. 16:00 C HS5 09:15 SR6 Dinca, D. 11:00 SR3 Cichocki, F. 09:15 HS2 Ding, M. 17:45 SR2 Clark, S. 16:00 HS6 Ding, Y. 17:15 SR6 Collins, A. 09:00 SR5 Dobranszki, C. 09:45 SR4 Cong, Y. 09:30 SR3 Doh, G. 10:30 SR6 Conversano, R. 10:00 SR6 Dominguez-Vázquez, A. 09:00 C SR2 09:45 HS6 10:15 SR6 Drobny, C. 14:00 SR6 09:00 C SR2 Coral, G. 11:00 SR4 15:00 HS6 Correyero Plaza, S. 10:00 HS2 Duchemin, O. 14:00 C SR6 09:00 SR6 Courtney, D. 16:45 SR5 09:00 C SR5 16:45 SR5 Eckhardt, D. 09:45 HS2 Cretel, C. 10:45 HS2 Edamoto, M. 15:45 HS3 Crofton, M. 18:00 HS2 17:15 HS5 Egawa, Y. 17:00 SR6 Cui, C. 09:30 HS5 Ehresmann, M. 14:30 HS2

We keep things moving on satellites!

Mechanisms from RUAG point Electric Thrusters, Solar Generators, Antennas and Instruments in the right direction. In extreme conditions. With utmost precision and reliability.

www.ruag.com/space @RUAGSpace 16 IEPC19 Programme Index E → H 17

Name A → Z Monday 16 Tuesday 17 Wednesday 18 Thursday 19 Friday 20 Name A → Z Monday 16 Tuesday 17 Wednesday 18 Thursday 19 Friday 20

Eichhorn, C. 10:00 HS5 Goebel, D. 14:00 C HS6 10:30 HS6 Elias, P.-Q. 09:30 HS3 Gole, H. 09:00 SR6 Fajardo, P. 09:45 SR2 Gómez, V. 17:00 HS2 Overview Fazio, N. 09:15 HS5 Gondol, N. 09:45 SR6 Feili, D. 14:45 SR3 09:00 C HS5 Gonzalez del Amo, J. 14:00 C SR3 10:00 Audimax Ferrato, E. 14:45 SR6 15:00 C SR3 Filleul, F. 16:00 HS6 González, J. 16:00 HS2 Frieman, J. 18:00 SR2 Gray, H. 15:30 HS6 Fruchtman, A. 10:15 HS6 Gray, T. 15:00 SR6 Funaki, I. 16:15 SR2 09:00 C SR6 Grimaud, L. 10:15 SR5 09:00 C HS3 Furukawa, T. 15:00 HS2 15:00 C HS2 Guarducci, F. 18:00 HS5 Furuya, R. 15:45 HS6 Guerrero, P. 10:00 HS6 17:30 SR2 10:30 HS6 Gabriel, S. 09:00 C HS6 09:00 C HS5 Guglielmi, A. 17:15 SR2 Gallud Cidoncha, X. 15:45 HS2 Guo, Y. 16:30 SR5 Garcia, V. 15:15 SR2 16:00 C HS6 Gurciullo, A. 15:30 SR2 10:15 HS6 Garrigues, L. 09:00 C HS6 09:00 C HS5 Habl, L. 10:45 HS5 15:00 HS6 10:15 SR2 Hakateyama, W. 17:15 HS2 Geng, J. 15:00 HS3 Hall, K. 09:15 HS5 17:45 SR4 Hall, S. 14:00 HS6 Georgin, M. 09:00 HS6 14:15 HS6 10:15 HS6 Hallouin, T. 09:00 C SR2 Gessini, P. 16:30 HS2 15:00 SR6 Gilpin, M. 09:00 SR5 15:45 SR6 Glascock, M. 16:00 SR4 09:00 C SR4 Ham, R. 16:30 HS6 Glogowski, M. 14:30 SR3 Hamada, A. 10:15 HS2

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E: [email protected] cobham.com T: +1716-667-6468 18 IEPC19 Programme Index H → J 19

Name A → Z Monday 16 Tuesday 17 Wednesday 18 Thursday 19 Friday 20 Name A → Z Monday 16 Tuesday 17 Wednesday 18 Thursday 19 Friday 20

Hang, G. 09:15 SR5 Hu, Ya. 09:00 C HS6 Haque, A. 14:15 HS2 Hu, Yo 09:30 HS5 Hara, K. 09:30 SR2 09:15 HS5 Huang, W. 18:45 SR2 Overview 11:15 SR2 Hugonnaud, V. 09:00 C SR5 Harmansa, N. 15:45 HS3 Huh, H. 16:15 SR5 Heidemann, R. 10:30 SR6 09:00 C SR2 Ichihara, D. 10:45 HS3 Henning, T. 15:15 SR5 Ide, S. 16:00 SR3 Hepner, S. 09:00 HS3 Ikeda, T. 10:45 SR6 Herdrich, G. 09:00 C SR3 09:45 HS3 Inaba, T. 15:15 SR4 09:45 SR3 Ito, G. 09:30 SR2 Herman, D. 09:45 SR6 Ivanov, S. 15:45 HS2 Hess, S. 11:00 SR2 Jackson, J. 16:15 HS3 Hey, F. G. 14:00 C HS2 17:30 HS2 Jakubczak, M. 09:15 SR2 Hiraka, K. 14:15 SR4 Jansen, F. 15:00 SR3 Hiroike, N. 14:15 HS5 Jarrige, J. 09:15 HS2 Hofer, R. 17:30 SR6 09:00 C SR2 Jia-Richards, O. 14:15 SR5 Hoffman, D. 10:30 HS5 Jia, Y. 15:00 HS5 10:30 HS6 Horisawa, H. 15:30 HS3 Johnson, I. 11:00 HS2 Hruby, V. 14:00 C HS2 09:15 SR4 Jorns, B. 14:00 SR6 15:15 SR5 16:00 C SR5 Junker, J. E. 09:00 SR3 Hsu, A. 16:00 C SR5

AEPS NEXT-C Advanced Electric NASA’s Evolutionary Xenon rocket.com Propulsion System Thruster - Commercial 20 IEPC19 Programme Index K → L 21

Name A → Z Monday 16 Tuesday 17 Wednesday 18 Thursday 19 Friday 20 Name A → Z Monday 16 Tuesday 17 Wednesday 18 Thursday 19 Friday 20

Kaganovich, I. 10:45 HS6 Krejci, D. 16:00 C SR5 11:15 SR5 Kamhawi, H. 16:00 C SR2 09:30 SR6 15:45 SR6 15:00 C SR2 15:00 C SR5 17:15 SR2 Kristinsson, B. 14:00 C SR5 15:15 HS3 Overview Kang, Q. 11:15 SR3 Kronhaus, I. 10:30 SR2 Kapulkin, A. 15:00 SR6 Kubota, K. 15:15 HS6 Karevsky, A. V. 09:00 SR3 Kumar, H. S. 10:45 HS2 Katsonis, K. 17:45 HS3 Kuninaka, H. 10:15 Audimax Kawashima, R. 15:00 SR2 La Rosa Betancourt, M. 16:45 SR3 Kazeev, M. 14:00 C SR4 09:15 HS3 Lafleur, T. 11:00 HS5 09:00 C HS5 Keerl, S. 09:30 SR5 Lascombes, P. 15:15 SR3 Kelly, C. 14:00 HS3 Laterza, M. 16:30 SR4 15:15 SR2 Kempkens, K. 15:45 HS6 18:00 SR4 Kerber, T. 14:30 SR2 Laube, J. 10:45 SR2 09:00 C HS3 Khmelevskoi, I. 11:00 SR6 Laufer, P. 17:30 HS6 Kim, M. 16:45 HS3 Lee, D. 09:30 SR6 Kim, V. 10:15 SR6 Leiter, H. 14:00 C HS5 09:00 C HS5 09:00 SR4 Kinefuchi, K. 10:15 SR6 16:45 HS5 Kitaeva, A. 09:00 C SR3 Lenguito, G. 14:00 HS2 10:00 SR3 15:45 SR3 Lev, D. 15:30 SR3 09:00 C SR3 10:15 SR3 09:30 SR4 Kolbeck, J. 15:00 SR4 09:45 HS5 Levin, D. 16:15 HS5 15:45 SR5 16:00 C SR4 16:30 HS5 Komarov, A. Lewis, R. 16:15 HS6 Komurasaki, K. 09:00 C SR2 Li, W. 14:45 SR2 Kottke, N. G. 15:15 HS6 LI, X. 15:00 HS3 Kozhevnikov, V. 15:00 C HS5 15:30 HS5 Li, Y. 15:15 SR3 15:45 HS5 Liang, S. 09:30 HS6 Kramer, A. 10:45 SR5 Ling, W. Y. L. 16:45 SR4 Little, J. 16:45 HS3 09:00 C HS2

Electric Propulsion Chemical Propulsion READY FOR TAKE OFF! Energy Systems Additive Layer Manufacturing Aerospace Engineering A unique Master‘s programme in Austriafhwn.ac.at/aero Testing Services ofﬁ [email protected] | fotec.at 22 IEPC19 Programme Index L → P 23

Name A → Z Monday 16 Tuesday 17 Wednesday 18 Thursday 19 Friday 20 Name A → Z Monday 16 Tuesday 17 Wednesday 18 Thursday 19 Friday 20

Liu, H. 10:15 SR2 09:00 C SR5 Nauschütt, B. 09:45 HS5 Liu, X. 16:15 SR5 10:00 HS3 Navarro Cavallé, J. 15:30 HS2 16:45 HS2 17:30 SR4 Neugebauer, C. 15:15 HS3 Overview Lobbia, R. 16:30 SR6 16:00 C HS6 Lopez Ortega, A. 09:45 SR2 Neugodnikov, S. 09:45 SR3 09:30 SR3 15:30 SR2 Neumann, A. 17:00 HS2 Lovtsov, A. 16:30 SR2 16:00 HS5 Neunzig, O. 09:00 C HS2 10:15 HS3 Lozano, P. 09:00 C SR5 Nguyen, T. T. H. 10:00 HS5 Lucken, R. 09:00 HS5 Ning, Z. 09:15 HS6 Lyne, C. 15:15 HS3 Ogunlesi, C. 10:15 SR4 Ma, C. 16:00 SR5 10:45 SR3 Oh, D. 09:00 C HS2 MacArthur, J. 10:00 SR5 Olano Garcia, A. 17:30 SR2 Magarotto, M. 10:30 SR3 09:00 HS2 10:00 HS2 Oshio, Y. 16:00 HS3 Mallon, M. 16:45 HS5 09:00 C HS5 Ottaviano, A. 09:15 HS3 Mani, K. V. 10:15 HS2 Packan, D. 09:00 C HS3 10:45 HS2 Markov, A. 15:00 SR6 Pan, R. 11:45 SR2 Marmuse, F. 17:15 HS3 Panelli, M. 11:00 HS6 Marrese-Reading, C. 09:45 SR5 Pavarin, D. 09:00 C SR3 Martín Ortega, Á. 15:45 SR2 Pedrini, D. 09:00 HS6 Martin, R. 15:00 SR2 Perales-Díaz, J. 17:30 HS5 Martínez Martínez, J. 09:45 HS5 Perez Luna, J. 09:00 HS5 Masillo, S. 11:15 SR6 Peterschmitt, S. 09:00 HS2 Massotti, L. 10:30 SR5 Peterson, P. 10:30 SR6 15:00 C SR5 15:00 C SR2 Matlock, T. 15:15 SR6 09:00 C SR6 16:00 SR6 Petro, E. 17:00 SR5 16:00 SR5 15:00 C HS5 16:30 HS2 Matsunaga, Y. 15:15 HS5 Matyash, K. 11:00 SR2 Mazouffre, S. 14:00 C SR2 09:00 C HS6 11:00 SR6 15:00 C SR6 McDonald, M. S. 09:45 HS6 Merino, M. 14:15 HS3 09:00 C HS3 Micci, M. 16:30 HS3 09:45 SR4 Develop Thrusters for GW Detection Mission 15:00 C SR4 Mikellides, I. 17:45 SR2 09:00 C SR6 09:00 C HS6 Mishra, A. 09:00 SR6 15:00 C SR6 17:30 SR6 Misuri, T. 16:45 SR6 15:00 C SR6 09:30 HS2 17:15 SR6 Moloney, R. 09:15 HS3 CALL FOR Monette, M. 16:30 HS3 Montag, C. 09:30 SR4 Mooney, M. 15:45 HS6 09:00 C HS2 IDEAS Morishita, T. 14:30 HS6 Mühlich, N. S. 09:15 SR5 AND Muranaka, T. 11:30 SR2 09:15 HS5 Murayama, Y. 16:15 SR3 Myers, R. 09:30 C Audimax TALENTS Nagamine, K. 16:15 SR6 Nakagawa, Y. 18:00 HS5 Nakayama, Y. 15:00 C SR6 09:00 HS3 Nakles, M. 10:45 SR6 Talk: Mon. 15:00 SR5 Nandyaca, H. 10:15 HS2 Natisin, M. 16:30 SR5 Exhibition at Hall 24 IEPC19 Programme Index P → T 25

Name A → Z Monday 16 Tuesday 17 Wednesday 18 Thursday 19 Friday 20 Name A → Z Monday 16 Tuesday 17 Wednesday 18 Thursday 19 Friday 20

Pintó Marín, F. J. 16:00 C HS2 10:30 SR3 Shimamura, K. 16:30 SR6 Polk, J. 15:00 HS3 15:45 HS5 Simmonds, J. 09:45 SR2 10:00 SR6 Polzin, K. 14:00 C SR4 Skalden, J. 09:00 SR4 Overview 15:00 C HS2 10:45 SR4 18:30 SR4 15:00 C SR4 Potrivitu, G.-C. 10:00 HS6 Smirnov, P. 17:15 HS6 10:15 HS6 Smirnova, M. 15:00 C HS5 16:15 HS5 Powis, A. 16:15 SR2 Smith, B. K. 10:30 Audimax Proulx, N. 15:30 SR6 Smolyakov, A. 16:00 SR6 09:00 HS5 Quraishi, A. 15:00 HS2 10:30 HS6 Raisanen, A. 10:00 SR2 Snyder, S. 09:15 HS2 Raitses, Y. 16:45 SR2 Sommavilla, T. 15:15 HS5 17:30 SR2 Sommerville, J. 17:00 SR2 Rakhimov, R. 15:30 HS5 Song, J. 10:30 HS2 Reeh, A. 17:00 HS5 Song, P. 15:00 SR5 Reeve, S. 09:45 HS6 Spears, R. 13:30 C Audimax Reissner, A. 09:30 Audimax Spemann, D. 11:30 HS3 11:00 C Audimax Staab, D. 10:15 HS2 Reitemeyer, M. 09:30 HS6 Starchenko, A. 09:15 SR3 Ren, J. X. 15:00 HS5 Steiger, C. 15:15 HS6 Richards, M. 09:30 SR3 Stesina, F. 16:15 HS2 Robinson, M. 10:00 SR4 Su, L. 14:30 SR6 Roessler, C. 09:00 C SR3 Surminskii, A. 11:30 SR3 10:15 SR3 Sutherland, O. 10:00 HS2 Rojas Mata, S. 15:00 C HS2 Swar, K. 16:15 HS2 Romano, F. 15:00 HS3 Taccogna, F. 10:45 SR2 Romei, F. 09:30 SR4 Tachibana, T. 15:45 SR4 Rongione, N. 09:00 HS2 Tahara, H. 15:00 C SR3 Rosati Azevedo, E. 10:30 HS2 Tajmar, M. 15:00 C HS3 09:45 SR5 09:30 HS3 Ross, J. L. 15:15 SR6 09:45 HS3 Ryan, C. 16:45 HS2 Takahashi, K. 14:00 C HS3 16:00 HS2 Sammut, M. 14:30 SR4 17:00 HS3 Samples, S. 10:45 HS5 Takahashi, M. 15:15 HS2 Sánchez-Villar, A. 10:15 HS3 Takao, Y. 14:00 SR5 Saravia, M. M. 14:00 C SR6 15:15 SR6 Sarrailh, P. 11:15 SR2 Sasoh, A. 11:15 HS3 Sato, Y. 14:00 HS5 Scharlemann, C. 10:00 C Audimax 11:00 SR5 14:00 C Audimax 14:00 C SR5 Scholze, F. 10:30 HS5 Schönherr, T. 09:00 C SR4 10:00 SR5 15:00 C HS3 Schwertheim, A. 09:30 HS3 Seifert, B. 16:00 HS2 09:00 C SR5 Sekine, H. 09:30 SR6 16:15 HS2 Proudly Supporting IEPC 2019 Shashkov, A. 16:45 SR2 Shaw, P. 18:15 SR4 09:15 SR2 Shen, Y. 10:30 SR4 Sheppard, A. 14:30 HS3 Shimhanda, S. 14:00 SR4 26 IEPC19 Programme Index T → Z 27

Name A → Z Monday 16 Tuesday 17 Wednesday 18 Thursday 19 Friday 20 Name A → Z Monday 16 Tuesday 17 Wednesday 18 Thursday 19 Friday 20

Takegahara, H. 14:00 C HS5 Yalin, A. 09:30 HS6 Tatsuno, A. 15:15 HS2 Yamakawa, Y. 09:45 HS2 Tauchi, S. 09:15 SR3 15:00 C HS2 Overview Taunay, P.-Y. 09:00 HS6 Yamamoto, N. 15:00 C SR2 09:00 HS6 Tavant, A. 10:00 HS6 Yamamura, T. 09:00 C HS2 Thomas, R. 17:45 HS5 Yamasaki, J. 16:30 SR6 15:30 SR3 Thompson, S. 16:00 HS6 09:00 C HS6 Yamashita, Y. 14:30 HS5 Thoreau, P. 09:45 HS2 Yang, L. 09:15 SR4 Thuppul, A. 09:30 SR5 Yang, W. 15:30 HS6 Tighe, W. 10:15 HS3 Yang, X. 10:00 HS2 Trescott, J. 15:15 HS2 09:00 C SR4 Yi, X. 16:00 C SR6 16:15 SR6 Trottenberg, T. 09:00 C HS3 Yim, J. 15:30 HS5 10:00 HS3 Yokota, S. 16:30 SR6 Tsikata, S. 10:00 HS5 Young, J. 10:00 HS6 Tsuchiya, M. 15:30 SR4 17:30 HS5 Tsukizaki, R. 09:00 HS5 Zarakovskiy, A. 16:45 HS6 Tsybulnyk, A. 09:45 SR3 Zhang, Y. 15:00 SR3 Turchi, P. 16:15 HS3 09:00 C HS3 Zhang, Z. 09:00 SR4 17:30 HS3 Uchizono, N. 09:15 SR5 Zheng, H. 15:00 HS5 Upadhyay, P. P. 09:00 C SR4 17:15 HS5 15:15 SR4 Zhou, C. 16:30 SR3 VanWoerkom, M. 18:30 SR2 Zhou, J. 09:45 HS3 Vaudolon, J. 16:30 SR6 Zhu, K. 10:15 HS5 Vaupel, M. 16:00 SR6 16:00 HS3 Zhu, X. 09:30 HS5 Vazsonyi, A. R. 10:45 HS6 Ziemer, J. 11:30 SR5 Velasco Valencia, R. 09:00 C SR3 Zitouni, B. 15:30 HS2 Viges, E. 17:45 HS2 16:45 HS2 Villafana, W. 14:00 C SR2 15:45 SR2 Zolotukhin, D. 16:15 SR4 Villemant, M. 15:00 SR5 15:15 SR2 Zurbach, S. 09:15 SR6 09:00 C SR6 Vincent, B. 15:30 SR6 Wachs, B. 09:15 HS2 Wada, A. 16:30 HS2 Walker, M. 13:30 C Audimax Wallace, N. 15:00 HS6 09:00 C HS2 Wang, G. 10:00 SR3 Wang, J. 15:30 SR5 Wang, Y. 10:45 SR3 Wang, Y.-F. 15:30 SR6 Watanabe, H. 09:00 C SR6 16:00 SR2 Wegner, T. 09:15 HS6 Wei, L. 09:15 SR2 15:00 C SR2 Weiss, S. 16:00 C SR2 Wen, X. 15:30 HS3 Wijnen, M. 09:30 HS2 Williams, J. 17:45 HS5 Winter, M. 15:30 HS3 15:00 C HS3 Wirz, R. 15:45 HS3 Woods, J. 14:45 HS3 09:00 C HS3 Wright, P. 15:30 SR5 Wu, P. 10:30 SR3 28 IEPC19 Programme Poster Session 29

Material Technology Hall Thrusters Ion Thrusters Pulsed Plasma Innovative Thruster Overview Explore the Poster Sessions Cathodes, Gimbals Thrusters Concepts Concepts at IEPC19 to get insight into A835 A131 A194 A133 A201 A162 Computer Modeling of Performance Character- A Thrust Balance for the Development of Commercial- Design and Construction of Studies on Helicon Plasma new technologies, current Non-Emission Electron Source istics and Interior Plasma MINOTOR ECR Thruster ly-Available Electrothermal a Rotating Magnetic Field, Thruster and Measurement with High Frequency Ionization Phenomena of High-Power S. Scharmann Pulsed Plasma Thruster Field-Reversed Configuration Methods developments as well as S. Roshanpour and High-Specific-Impulse Systems for Powered Flight of (RMF-FRC) Thruster D. Kuwahara Micro/Nano-Satellites at Osaka Hall Thrusters for In-Space A250 C. Sercel different matters regarding Propulsion Institute of Technology A 3D Hybrid-IFE-PIC-MCC mod- A416 H. Tahara Electric Propulsion. H. Tahara el for the discharge chamber A286 1-D PIC Model of a Magnetically Resistojets/Arcjets simulation of ion thrusters Investigation of Antenna Enhanced Plasma Thruster A334 A134 Current and Regime Transition Poster Sessions at the Main Exhibition Site Y. Cao M. Minute Low frequency ionization Development of the Osaka in Electrodeless Inductive th Monday 16 / 12:30 – 14:00 A132 Institute of Technology 2nd Plasma Generators oscillation model with A256 A483 Thursday 19th / 12:00 – 14:00 Study on Low-Power azimuthal dimension in a Hall PROITERES Nano-Satellite with R. Georg 2D Particle-in-Cell Simulation Numerical Simulations of Water-Cooled and thruster High-Power Electrothermal Anode-Radiation-Cooled DC of Current Characteristics in Pulsed Plasma Thrusters for a Capacitively Coupled RF J. Bak A414 Arcjet Thrusters Using HAN and Three-Grid Ion Optics Powered Flight Micro-Thruster Numerical Investigation Water Propellants with Special A. Sun H. Tahara A. Popoli Vaporing Systems A490 of Ignition in a Novel Positron-Catalyzed Fusion H. Tahara A PIC/MCC simulation on the A335 A866 initial ignition stage of a 20mN A135 Propulsion Concept Feasibility study of sublimable Basic Characteristics of Plasma Hall thruster Research of Debris Removal L. Brieda substance as an alternative Thruster using ICR Heating in J. Yizhou Systems by Electric Propulsion propellant to xenon in ion and Development of the 4th Sheet Plasma A486 MPD Thrusters thrusters PROITERES Nano-Satellite for A. Tonegawa A570 M. Adachi Its Practical Space Experi- Characteristics of laser sustained plasma using argon Development of a 200 W Class ments at Osaka Institute of A809 A130 Hall Thruster for an Active and methane for on board A807 Technology Experimental Evaluation of Performance Characteristics Debris Removal System laser-based thruster Combined optical emission and H. Tahara the Micro Water Thruster of High-Power Steady-State M. Matsui N. Yamamoto laser absorption spectroscopy Recovering Waste Heat of a MPD Thrusters with Divergent of Xenon gridded ion thruster Spacecraft and Cusp Magnetic Fields A231 A587 A568 Using Permanent Magnets for R. Kozakov Longterm testing and evalua- K. Nishii Metallic Vapor Thruster In-Space Propulsion Fluid simulation of low tion of the vacuum arc thruster frequency oscillations in Hall using Field-emitted Electron H. Tahara system using multi-element thrusters cathodes Bombardments A. Rostek P.-Y. Chang A813 M. Kuehn Field Emission / Integrated simulation solutions A674 A799 Colloid Thrusters for the plasma and transversal A269 Thermal analysis of diode-laser physics in electric propulsion 2D (axial-azimuthal) Parti- Evaluation of Coaxial Short- coupled fiber-tip heat A803 systems cle-In-Cell benchmark for ExB pulse Laser-assisted Pulsed discharges Plasma Thrusters source for high-temperature Probe study on ion beam and M. Kubecka generation T. Charoy K. Sato backflow for different electric T. Matsuo propulsion technologies V. Hugonnaud A716 A438 Study of the electron anoma- Global Strategic Study of two-stage pulsed lous transport in a Hall effect plasma thruster with special A857 Investments and thruster using a 2D multi-fluid propellant combined ion liquid Molecular Dynamics Simula- Long-Term Planning simulation and resin manufactured by 3D tions of Nanodroplet Break-up K. Hara printer for Ionic Liquid Electrospray Thrusters A350 J. Saiki Y. Takao Overview of SITAEL Electric Propulsion Developments T. Misuri MONDAY 32 IEPC19 Programme Monday 16 33

Wecome Speech Audimax 09.00

David C. Byers Memorial Lecture → see page 10 Audimax Moderated by Roger Myers 09.30

Plenary Lecture with Agencies → see page 10 Audimax Electric Propulsion for Future Science and Exploration

10.00 Moderated by Carsten Scharlemann

Panel Discussion → see page 10 Audimax EP in the Commercial Space Area / Moderated by Alexander Reissner Monday 11.00

Lunch Break & Poster Session 12.30

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

HS6 SR5 SR6 SR2 HS5 SR4 HS2 SR3 HS3

1st Chair D. Goebel 1st Chair C. Scharlemann 1st Chair O. Duchemin 1st Chair S. Mazouffre 1st Chair H. Leiter 1st Chair K. Polzin 1st Chair V. Hruby 1st Chair J. Gonzalez del Amo 1st Chair J. Brophy 2nd Chair G. Beratti 2nd Chair B. Kristinsson 2nd Chair M. Saravia 2nd Chair W. Villafana 2nd Chair H. Takegahara 2nd Chair M. Kazeev 2nd Chair F.Hey 2nd Chair M. Andrenucci 2nd Chair K. Takahashi

A299 A149 A129 A532 A154 A185 A303 A189 A202 The Effect of Anode Development of Hybrid Data-Driven and Spatiotemporally Three-Dimensional Parti- A Performance Comparison of Versatile Xenon Flow Controller Activities of the H2020 Strategic Performance Scaling of Position on Operation of a Ionic Liquid Electrospray Physics-Based Model for Resolved Ion Velocity cle Simulations of Electron solid Propellants in a Surface Arc for Extended Hall Effect Thruster Research Cluster on Space Drag-Modulated Plasma 25-A class Hollow Cathode Thrusters with a Massive Plasma Turbulence in a Distribution Measure- Extraction for a Miniature Thruster: Sulfur and Teflon Power Range Electric Propulsion (2015-2019) Aerocapture S. Hall Emitter Array for Higher Hall Effect Thruster ments in the 12.5 kW Microwave Discharge S. Shimhanda G. Lenguito J. Gonzalez del Amo C. Kelly 14.00 Thrust Density B. Jorns HERMeS Hall Thruster Neutralizer Using Water as Y. Takao V. Chaplin the Propellant Y. Sato

A300 A173 A147 A531 A309 A556 A721 A711 A254 The Effect of a Hall Laboratory Demonstration Modular Comprehensive Ion Velocity Measure- Lifetime Evaluation of Performance Evaluation and Development of an additively The Importance of Electric Fluid-kinetic propulsive magnetic Thruster-like Magnetic of a Staging System for Modeling of Plasma ments in the Magnetically Microwave Discharge Development of Air Bearing manufactured mass, volume Propulsion to Future Exploration nozzle model in the fully-magnet- Field on Operation of a Electrospray Thrusters Behavior in Hall Thrusters Shielded Miniature Hall Neutralizer using Thrust Measurement System of and cost optimised fuel tank of the Solar System ized limit 25-A class Hollow Cathode O. Jia-Richards T. Andreussi Thruster (MaSMi) Using Numerical Analysis Surface Arc Thruster for microsatellite propulsion J. Cassady M. Merino 14.15 S. Hall Laser-Induced Fluores- N. Hiroike K. Hiraka systems MiniTank cence A. Haque V. Chaplin

A557 A225 A204 A513 A218 A616 A456 A753 A420 Development of a Colloid Micro-Thruster Model for the Increase in Charge Exchange Numerical study of Development of Pulsed Plasma Progress in Automated System Application of Solar Electric Theoretical scaling laws for Microwave Discharge (CMT) Component Thruster Efficiency from Collision in the Plume of microwave discharge ion Thruster for a Pico-Satellite Design by Evolutionary Algo- Propulsion in the Emerging water-vapor propellant thrusters Cathode for a 200 W Class Development Testing Cross-Channel Coupling a 200 W Laboratory Hall thruster µ10 M. Sammut rithms Satellite Servicing Industry A. Sheppard

14.30 Hall Thruster Towards Meeting LISA in Nested Hall Thrusters Thruster Y. Yamashita M. Ehresmann M. Glogowski T. Morishita Mission Requirements L. Su T. Kerber N. Demmons

A372 A459 A220 A899 A253 A876 A717 Pure Ionic Electrospray Magnetic Circuit Study on the Influence Fiber-fed Pulsed Plasma Thruster An overview of French electric Propulsion subsystem for a stand Validation of an Equivalent Circuit Extractor Design Optimization for Hall of Electron Conduction (FPPT) for Small Satellites propulsion activities at CNES alone interplanetary CubeSat Model for Rotating Magnetic Field Optimization Thrusters Design Paths on the Ignition D. Carroll C. Boniface D. Feili Field-Reversed Configuration 14.45 R. Antypas C. Ferrato Process of Hall Thruster Thrusters W. Li J. Woods Plenary Lecture Audimax European National Agencies 14.00

34 IEPC19 Programme Monday 16 35

HS6 SR5 SR6 SR2 HS5 SR4 HS2 SR3 HS3

A629 A284 A470 A276 A272 A657 A826 A275 1st Chair M. Tajmar Development of a C12A7 Micro-Newton Electros- Theoretical Models of Experimental Investiga- Hybrid-PIC Simulation of A Vacuum Arc Ion Thruster for HEMPT-Strategy to address High power electric propulsion: 2nd Chair J. Polk Electride Hollow Cathode pray Thrusters for China’s Suppression of Instabil- tion of the Implications Back-sputtered Carbon SmallSat Applications current and future Space Market MARS plus EUROPA - already and Joint Operation with Space-Borne Gravitational ities in Hall Thruster by of Nesting Multiple Hall Transport in electric J. Kolbeck J. Degremont beyond 2025! A176 Plasma Thrusters Wave Detection Mission Shear of Magnetic Field Thruster Channels propulsion test facility F. Jansen Effects of magnetic shielding on 15.00 C. Drobny (Tian Qin) A. Kapulkin S. Cusson H. Zheng the performance of Multi-cusped P. Song field thruster J. Geng

A644 A344 A278 A288 A302 A860 A212 A418 A243 Monday Comparison of the thermi- Characterisation of A Comparison of Possible EP system development EMC considerations for RIT Optical measurements of ablation The Benefits of Continued Electric Propulsion for Small Electric Propulsion Pointing onic emission properties electrospray microemit- Mechanisms for Facility and functional validation engines based on 3D full- process of double-cylindrical Advances in the Propulsive Satellites: A Case Study Mechanism EPPM for the of LaB6 and C12A7 ters fabricated by planar Effects on Hall Thruster tests for the Electra GEO wave field simulation of pulsed plasma thruster Capability of the Electric GEO P. Lascombes Spacebus Neo Platform

15.15 N. G. Kottke and 3D photolithography Operation satellite electromagnetic emission T. Inaba Communications Satellite C. Neugebauer T. Henning T. Matlock V. Garcia of their RF coils J. Trescott T. Sommavilla

A482 A650 A306 A142 A496 A210 A607 A398 Development of High A Novel Variable Mode A comprehensive xenon Hall thrusters develop- Numerical simulation of EP orbit raising: environmental VENUS – Updates on Technologi- Modeling, Simulation and Testing Current LaB6 hollow Emitter for Electrospray collisional-radiative ment at Exotrail: pres- plasma discharge in RF ion effects impact on satellites, cal Mission Using IHET of a Magnetically Enhanced RF Cathode Thrusters model of atomic and ionic entation and experimental thruster modelling and challenges D. Lev Plasma Source for a High Power

15.30 W. Yang P. Wright excited levels for Hall investigation R. Rakhimov B. Zitouni Electromagnetic Thruster thruster A. Gurciullo X. Wen Y.-F. Wang

A695 A883 A547 Featherweight Heaterless More added value? – an investi- Electric Propulsion Activities Hollow Cathode Charac- gation on the commercial benefit at the UCLA Plasma Space terization of different EP technologies for Propulsion Laboratory

15.45 M. Mooney orbital propulsion instancing R. Wirz H2020´s GIESEPP C. Dietz

1st Chair V. GGarcia 1st Chair D. Krejci 1st Chair J. Boeuf 1st Chair S. Weiss 1st Chair S. Ciaralli 1st Chair J. Kolbeck 1st Chair E. Bosch 2nd Chair C. Neugebauer 2nd Chair A. Hsu 2nd Chair X. Yi 2nd Chair S. Arali 2nd Chair – 2nd Chair B. Che 2nd Chair F. Pintó Marín

A768 A223 A762 A791 A905 A421 A790 A564 Evaluation of Iodine Direct Thrust Meas- Stationary Profiles and Performance Comparison Analytical and numerical Performance and Efficiency of Development of a 100 mN Experimental Study of Traveling Compatible Hollow urement and Plume Axial Mode Oscillations of a 2 kW Hall Thruster simulation of Ring Cusp Electric Solid Propellant in a Horizontal Torsion Balance Wave Plasma Acceleration and

16.00 Cathode Configurations Characterization of a in Hall Thruster with Heaterless Cathodes Discharge Chamber Pulsed Plasma Thruster B. Seifert Optimization of Magnetic Field S. Thompson Porous Electrospray A. Smolyakov Mounted on the Outer F. Cannat M. Glascock Structure for Electrodeless RF Thruster Pole Piece and on the Plasma Thruster C. Ma Thruster Centerline Y. Oshio T. Andreano

A802 A471 A681 A441 A367 A659 A413 A766 Diagnostic analysis of a Development and Status of Research Development Status of Plasma characteristics Micro-cathode arc thruster Design and testing of a μN Design of an Experiment for Com- 30 A heaterless hollow Characterization of an Activities on Electric 6-kW-class Hall Thrusters in the backflow region of improvement by the second MPD - mN torsional thrust balance pression and Nozzle Expansion of cathode Ionic Liquid Electrospray Propulsion at CIRA at JAXA ion thruster plumes using stage with wireless microwave power a Field-Reversed Configuration

16.15 A. Daykin-Iliopoulos Thruster with a Porous F. Battista I. Funaki kinetic and electron fluid D. Zolotukhin transmission for Advanced Space Propulsion Metal Blade Array models K. Swar P. Turchi X. Liu D. Levin 36 IEPC19 Programme Monday 16 37

HS6 SR5 SR6 SR2 HS5 SR4 HS2 SR3 HS3

A890 A522 A241 A342 A529 A662 A784 A785 Characterization of a Performance of a Fully PPS®X00 Hall Thruster Parametric study of Study of Ion Thruster Experimental Analysis of Cusped TIDBIT - Thruster In-Space Electromagnetic Propulsion Using Fixed-Volume Release Conventionally Machined Development Status at 1,5- and 2.5-kW Hall Backflow Characteristcs Magnetic Field Focusing on Diagnostics with Bus Integrated Non-Ionized Dipole Gases System for Initiating an Arc Liquid-Ion Electrospray Safran Thrusters with an external with Neutralization Using Vacuum Arc Thrusters Telemetry M. Micci

16.30 Discharge in a Heaterless Thruster Operated in PIR J. Vaudolon discharge zone Kinetic PIC-DSMC M. Laterza T. Matlock Hollow Cathode M. Natisin A. Lovtsov D. Levin R. Ham

A422 A787 A655 A392 A804 A798 A211 A848 The development of the Reconstructing Elec- SITAEL HT100 Thruster, Laboratory tests of Theoretical and Experi- An investigation of alternative Thrusters modelling, propellant Low-Field Mode Transitions in a Integrated Thruster Unit trospray Plume Current Full Ground Qualification 10.5kW Hall thruster with mental assessment of Ion propellants for pulsed plasma choice and plume expansion: Spiral-Antenna Helicon Thruster Monday ITU100 and ITU140 Spatial Distributions using T. Misuri external layer Extraction phenomena thrusters openPlumeEP capabilities J. Little 16.45 A. Zarakovskiy Computed Tomography A. Shashkov M. Mallon W. Y. L. Ling B. Zitouni D. Courtney

A289 A794 A825 A740 A612 A554 A123 A852 Development and Investigation of Electros- Development status of Performance of the Aurora Elegant Approach for Ignition Capability of Pulsed Cryopumping Challenges of Laboratory demonstration of Qualification of an Electric pray Plume Composition SITAEL’s 20kW class Hall Low-Power Hall Effect solving the Conservation Plasma Thruster with Green EP-Propellants in DLR’s Electric a bidirectional helicon plasma Propulsion Thruster during Voltage Transients thruster Thruster Laws in Global Modelling Liquid Propellant Propulsion Test Facility thruster for space debris removal

17.00 Orientation Mechanism for E. Petro T. Andreussi J. Sommerville of Radio-Frequency Ion J. Aoyagi A. Neumanni K. Takahashi the Electra GEO satellite Thrusters V. Garcia A. Reeh

A840 A590 A885 A910 A699 A898 A796 A933 Research and develop- Interaction of Droplets in SITAEL’S HT400 Performance, Stability, Three-dimensional Micro-Cathode Matrix Arc Development of Propulsion Lodine as propellant for electric ment of radio-frequency Electrospray Plumes Hall-Effect Thruster for and Wear Characteriza- simulation of ion Thrusters- A Modified Approach Testing and Integration Facilities propulsion: optical measurements cathode-neutralizer Constellation Applications tion of a Sub-Kilowatt Hall thruster plume-spacecraft to Micro-Cathode Arc Thrusters at Canon Electronics of I density and temperature,

17.15 M. Davis P. Smirnov T. Misuri Thruster interaction using EX-PWS K. Daniels W. Hatakeyama comparisons to a global model H. Kamhawi H. Zheng F. Marmuse

A477 A193 A216 A491 A321 A656 CNT-based cold electron The 12.5 kW Hall Effect Performance of a Studying the formation Experimental Study on Ignition Inter-Laboratory Comparison: source for space applica- Rocket with Magnetic 100-Watt Radial Scaled and neutralization of an Reliability of Pulsed Plasma Tests of a single thruster in tions on nano-satellites Shielding (HERMeS) Thruster with Anode Layer ion thruster plume with Thrusters two different facilities, on two 17.30 P. Laufer R. Hofer A. Olano Garcia EP2PLUS X. Liu different thrust balances J. Perales-Díaz F. G. Hey

A266 A410 A854 A536 A653 A 30-kW Class Magneti- Mechanism Behind the Neutral Density Simulation The study on the lifetime of the University of Michigan’s cally Shielded Nested Hall Dependence of Thrust in the Grid Region of Ion micro cathode arc thruster Upgraded Large Vacuum Test Thruster on Facility Backpressure Thrusters using the ffx Ion J. Geng Facility S. Cusson and Implications on the Optics Code E. Viges 17.45 Operation of the SPT-140 J. Williams Onboard the Psyche Mission I. Mikellides 38 IEPC19 Programme Monday 16 39

HS6 SR5 SR6 SR2 HS5 SR4 HS2 SR3 HS3

A714 A834 A661 A847 Impact of Facility Development of a 3D ion Influence of Insulator Geometry Improved Pumping Speed of Pressure on the Wear of optics modelling code on Vacuum Arc Thruster Lifetime Custom Cryopumps for Electric the NASA HERMeS Hall F. Guarducci M. Laterza Propulsion Vacuum Facility 18.00 Thruster M. Crofton J. Frieman

A630 A169 Data-driven Models for Predicting Pulsed Plasma the Effects of Background Thruster Performance with Deep Pressure on the Operation Recurrent Networks Monday 18.15 of Hall Thrusters P. Shaw M. Byrne

A664 A893 Test Results of ExoTerra's Pulsed Plasma Acceleration Halo Electric Propulsion Modeling in Detonation and

18.30 Module Deflagration Modes M. Vanwoerkom K. Polzin

A713 Variation in Ion Acceleration Character- istics of the HERMeS Hall

18.45 Thruster during Magnetic Optimization W. Huang

Session End 19.00 TUESDAY 42 IEPC19 Programme Tuesday 17 43

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

HS6 SR5 SR6 SR2 HS5 SR4 HS3 SR3 HS2

1st Chair S. Mazouffre 1st Chair D. Courtney 1st Chair T. Matlock 1st Chair R. Hofer 1st Chair E. Bosch 1st Chair T. Schönherr 1st Chair J. Cassady 1st Chair D. Lev 1st Chair K. Dannenmayer 2nd Chair S. Thompson 2nd Chair B. Seifert 2nd Chair H. Watanabe 2nd Chair K. Komurasaki 2nd Chair D. Feli 2nd Chair M. Glascock 2nd Chair J. Woods 2nd Chair C. Roessler 2nd Chair O. Neunzig

A628 A213 A140 A879 A678 A497 A361 A187 A242 Experimental characterization of Quantitative mapping of the Development of a 1.5KW High SITAEL’s Magnetically Shielded Global model of a Investigation on the Directed-Energy Study of Operation of Digital Filtering of Electric the attachment length in orificed mechanisms affecting electros- Specific Impulse Magnetic 20 kW Hall Thruster Tests magnetized ion thruster Discharge Arc Behaviour Propulsion Architecture Power and Propulsion Thruster Time Domain hollow cathodes pray thruster lifetime Shielded Hall Thruster T. Andreussi with xenon and iodine of an Asymmetric for Deep-Space Missions System based on Closed Radiated Emissions P.-Y. Taunay A. Collins A. Mishra R. Lucken Electrodes Pulsed with Characteristic Velo- Brayton Cycle Power N. Rongione 09:00 Plasma Thruster cities of Order 100 km/s Conversion Unit and Z. Zhang J. Brophy Electric Propulsion A. V. Karevsky

A663 A368 A274 A591 A831 A108 A458 A270 A521 Two-Photon Absorption Laser Resolving electrospray emission High Throughput 1.5 kW Preliminary tests of HIKHET Investigation on Analysis of Distributed Hybrid Electric Propulsion Electric Propulsion Direct thrust measurement Induce Fluorescence (TALIF) of modes using high-speed current Hall Thruster for Satcoms laboratory model at IPPLM Alternative Propellants for Energy Release Charac- System on the Basis of Mission Design with of a vacuum arc thruster Neutral Xenon Density in a Barium measurements S. Zurbach M. Jakubczak Gridded Ion Engines teristics in an Ablative SPT and PPT Minimal Solar Cells J. Jarrige 09.15 Oxide Hollow Cathode Plume N. Uchizono N. Fazio Pulsed Plasma Thruster M. Kazeev Radiation Degradation T. Wegner L. Yang A. Starchenko

A689 A571 A901 A343 A862 A476 A190 A595 Fiber Coupled Cavity Enhanced Spatially-Resolved Electrospray Development of the High Voltage Effects of Thrust Noise on Integrated Vlasov-Fully PETRUS 2.0 PPT and High Efficiency Auto Mechanically amplified Thomson Scattering Diagnostic Plume Current and Mass Flux Hall Accelerator Propulsion Drag-Free and Attitude Kinetic PIC Simulations of its CubeSat-size PPU: Resonant Converter milli-Newton thrust

for Use in Electric Propulsion Measurements and Analysis System Control System Plasma Plumes Testing and Characteri- Anode Power Supply balance for RF-thrusters Tuesday

09.30 Facilities A. Thuppul H. Kamhawi K. Cui C. Cui zation Design, Development M. Wijnen A. Friss C. Montag Testing M. Richards

A760 A892 A651 A377 A882 A931 A346 A715 5-100 A LaB6 Hollow Cathodes Characterization of Electrospray The Application of an Advanced Mini-CHT powered Formation Influence of Hollow Cath- Development of an Designing, Manufacturing Development of the for High-Power Hall Thrusters Thruster Electrode Overspray Electric Propulsion System on Flying Mission for Magnetic ode design parameters Electrostrictive Force and Testing of Power SPACE Lab Thrust Stand G. Becatti and Backspray the NASA Power and Propulsion Reconnection Research in Space on Ring Cusp Discharge Feeding Subsystem for Processing and Control for Millinewton Thrust

09.45 C. Marrese-Reading Element (PPE) J. Simmonds Chamber performances Liquid Pulsed Plasma Unit for a 1.5 kW Hall Measurement D. Herman F. Cannat Thruster Effect Thruster P. Thoreau C. Dobranszki S. Neugodnikov

A427 A909 A282 A280 A578 Mode Transition in a LaB6 Hollow Microfluidic and materials Overview of the Ascendant Deep Space Power Self-calibration Laser Cathode for Electric Propulsion improvements in the ion Sub-kW Transcelestial Electric Processing Unit for the Induced Fluorescence Systems for Small Satellites Electrospray Propulsion System Propulsion System (ASTRAEUS) Psyche Mission technic in Electric Propul- 10.00 G.-C. Potrivitu J. MacArthur R. Conversano G. Lenguito sion plasma diagnosing X. Yang

A428 A283 A409 A863 Systematic Testing of Improved Development Acceptance Design and Implemen- Laser ablation plasma Designs of Miniaturized LaB6 Testing of the Thruster Compo- tation of a High Voltage diagnostics for electro- Hollow Cathodes for Electric nent of the Ascendant Sub-kW Supply for Gridded Ion static acceleration

10.15 Propulsion Systems for CubeSats Transcelestial Electric Propulsion Thrusters using model- A. Hamada and Small Satellites System (ASTRAEUS) based control algorithms G.-C. Potrivitu R. Conversano C. Roessler

A369 A873 A419 A623 Lithium Hollow Cathode for Development of a low power REGULUS: Know-How Active Wave Injection a Very High Isp Interstellar HEMP Thruster EV0 Acquired on Iodine Diagnostic for Plasma Precursor Ion Thruster R. Heidemann Propellant Dispersion Relation 10.30 D. Goebel M. Magarotto Measurements E. Choueiri

A371 A878 A538 High Current Hollow Cathode HT5k Thruster Unit Development Torsional Balance Thrust for the X3 100-kW Class Nested History, Status and Way Forward Measurement Techniques

10.45 Hall Thruster T. Andreussi for Small RF Thrusters G. Becatti C. Cretel

Conference Tour 11.00 WEDNESDAY 46 IEPC19 Programme Wednesday 18 47

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

HS6 SR5 SR6 SR2 HS5 SR4 HS3 SR3 HS2

1st Chair S. Gabriel 1st Chair P. Lozano 1st Chair I. G. Mikellides 1st Chair A. Dominquez 1st Chair H. Leiter 1st Chair P. P. Upadhyay 1st Chair P. Turchi 1st Chair R. Velasco Valencia 1st Chair T. Yamamura 2nd Chair L. Garrigues 2nd Chair V. Hugonnaud 2nd Chair S. Zurbach 2nd Chair C. Drobny 2nd Chair M. Mallon 2nd Chair – 2nd Chair D. Packan 2nd Chair D. Pavarin 2nd Chair J. Little

A782 A139 A906 A156 A356 A224 A158 A474 A415 Recent Advances in Low-Current Dual-Axis Torsional Thrust Qualification Status of the PPS® Convergence of Stochastic T7 thruster design and Electrostatic Probe Optimum design for Development of a Numerical Model of a Hollow Cathodes at SITAEL Stand for Simultaneous Direct 5000 Hall Thruster Unit Models for Electric Propulsion performance Investigation of Very Low the drive-coil of a 500J full bridge series Magnetically Enhanced D. Pedrini Measurement of Thrust and O. Duchemin Plume Simulation J. Perez Luna Power Arcjet VELARC inductive pulsed plasma resonant radio-frequency Plasma Thruster

09:00 Mass Loss S. Araki in IRS and ESA-ESTEC thruster and its numerical generator for optimized M. Magarotto M. Gilpin Facilities evaluation RIT operation J. Skalden B. Che J. E. Junker

A207 A445 A673 A222 A688 A122 A191 A512 A460 Tests of an iodine-fed rf-neu- Development of a Retarding Qualification status of the Long-term Scale Characteristics T5 Performance, Indus- An Efficient Ionization Effects of Collisional-Ra- High Voltage Power 3D simulations of a tralizer Potential Analyser for Low EP system for Heinrich Hertz of Low-frequency Oscillation of trialisation and Future Method for Pressure Up diative Processes with Supply for T5 Gridded Ion magnetized Hall Effect P. Dietz Density FEEP Thruster Beam satellite (H2Sat) Hall Thrusters Applications To Thousands of Pascals Relative Drift in Electric Thruster thruster plume 09.15 Diagnostics S. Ciaralli L. Wei K. Hall L. Chang Propulsion Devices M. Blaser F. Cichocki N. S. Mühlich R. J. Abrantes

A896 A566 A599 A235 A360 A170 A259 A567 A564 Ariane Group 5A Neutralizer Two-dimensional plasma plume Development and Performance Study of Xenon Wall Accommoda- Testing of a 50,000-s, The Development and Water as an Alternative Design and Manufactur- Investigation of the Circuit qualification status density characterisation of the Test of a 50 W-class Hall thruster tion Model and Background Flow Lithium-fueled, Gridded Qualification of the STAR Propellant for a Next ing of Control Unit for low and Ablation Model for a M. Berger IFM Nano Thruster D. Lee During Hall Thruster Ground Test Ion Thruster Resistojet System for Generation Plasma and medium power Hall Vacuum Arc Thruster

09.30 S. Keerl G. Ito J. Brophy Telecommunications Propulsion System Effect Thruster S. Bai Applications A. Schwertheim S. Neugodnikov F. Romei

A297 A260 A634 A263 A811 A786 A330 A575 A573 Performance Testing of a MEMS FEEP Thrusters – Minia- Development and Characteri- Numerical Investigations of Development and testing A 17.8-GHz Ammonia Numerical Simulations Development of High Numerical Analysis of Microwave ECR Neutralizer for turised Liquid Metal Ion Source zation of a Miniature Hall-Effect Background Pressure Effects and of the NPT30 ion iodine Microwave Electrothermal of the Plasma Discharge Efficiency Power Plasma Acceleration the X-EPT Gridded Ion Thruster using Glass Capillaries Thruster using Permanent Channel Erosion in the SPT-140 thruster Thruster for CubeSats and in an Helicon Plasma Processing Unit for Hall Driven by Loop Coil in Wednesday

09.45 for Telecoms Applications M. Tajmar Magnets Hall Thruster for the Psyche J. Martínez Small Satellites Thruster Thruster Electrodeless Thruster S. Reeve N. Gondol Mission M. Micci J. Zhou A. Tsybulnyk Y. Yamakawa A. Lopez Ortega

A172 A362 A375 A247 A383 A393 A560 A584 A818 LaB6 hollow cathode work Development, Production, and Miniaturized Cylindrical Hall Numerical Simulations of AFRL Development of 50 W Lifetime Investigations of Research on Micro Power Processing Unit Effect of the initial function enhancement: insight Testing of the IFM Nano FEEP Thrusters EP/TEMPEST experiment class RF gridded ion an Additively Manufac- Impulse Measurement Activities at Thales Alenia electron distribution into the chemical processes Thruster J. Simmonds using the Thermophysics Unified thruster tured High-temperature Technology for Micro Space in Belgium function in magnetic

10.00 P. Guerrero T. Schönherr Research Framework (TURF) T. Nguyen Resistojet Heat Exchang- Cathode Arc Thruster E. Bourguignon nozzle expansions L. Brieda er from Tantalum X. Liu S. Correyero Plaza M. Robinson

A245 A675 A465 A237 A446 A403 A633 A729 A744 Plasma model and experimental The IFM Micro FEEP thruster: Investigation of the possibility to Study on Feed System of Iodine Development Status of Structural effects on PIC/fluid/wave simu- Rafael's Power Process- A 3D Numerical Study of investigation of a hollow cathode a modular design for smallsat develop competitive small power Cusped Field Thruster Microwave-ion Thruster the high temperature lations of the plasma ing Unit (PPU) for Electric Arcjet Thrusters: Effect of neutraliser propulsion stationary plasma thruster (SPT) H. Liu M5 for Small and Micro performance of the discharge in an ECR Propulsion Systems Electrode Configuration A. Gurciullo L. Grimaud V. Kim Satellites Super High Temperature plasma thruster D. Lev on Performance of Arcjet 10.15 K. Zhu Additive Manufactured A. Sánchez-Villar thruster Resistojet (STAR) H. Nandyala C. Ogunlesi

A301 A686 A836 A285 A652 A631 A888 A609 Hollow cathode thermal model- The ESA Earth Observation Pro- Overview of NASA's Solar Electric Influence of additional electric Discharge-Mode Testing Effect of structure AIRBUS DS PPU Discrete Boltzmann ling and self-consistent plasma gramme activities for the design, Propulsion Project field on discharge performance of the X-EPT Microwave characteristics on qualification status for Modeling of Atmospheric solution: two step neutralization development and qualification of P. Peterson of Hall thruster under internal and ECR Gridded Ion Thruster start-up process of an HET, GIT and New Space Pressure Plasma Jet

10.30 modelling the mN-FEEP thruster external cathode position studied for Telecoms Applications Arcjet thruster Technologies J. Song P. Guerrero L. Massotti by particle-in-cell simulation D. Hoffman Y. Shen F. Pintó Marín X.-F. Cao 48 IEPC19 Programme Wednesday 18 49

HS6 SR5 SR6 SR2 HS5 SR4 HS3 SR3 HS2

A331 A779 A294 A143 A225 A913 A795 An Axisymmetric Direct Kinetic Development of low-power micro EP plasma plume in orbit: Diag- Development of the Development Progress Development of a High Numerical Simulation and Solver for Simulation of Hollow cylindrical hall thruster “SCHT-1” nostics and analysis correlation Miniature Xenon Ion of an Adaptable Deorbit Voltage Power Process theoretical analysis of Cathode Plasmas T. Ikeda J. Laube Thruster with Hollow System for Satellite Unit for a CubeSat Particle Acceleration in

10.45 A. R. Vazsonyi Cathode Operation Constellations Electrospray Thruster Traveling Magnetic Field S. Samples J. Skalden C. Ma Thruster H. S. Kumar

A452 A805 A776 A639 A390 A930 A Plasma Model for Orificed CLIMB: Exploration of the Van Characterization of a 100 Coupling of an all-electric Performance Theory 13kW Advanced Electric

Hollow Cathodes Allen Belt by CubeSats A-class LaB6 hollow cathode for spacecraft with its plasma plume and Development of a Propulsion System M. Panelli C. Scharlemann high-power Hall thrusters and its environment Resistojet Based Hybrid Power Processing Unit 11.00 S. Mazouffre S. Hess Electro-Chemical Thruster Development G. Coral E. Soendker

A914 A724 A627 A833 A937 Validation of a drift diffusion Recent flight data of the IFM Experimental investigations and Simulation of plasma plume Research on a controlled model for a hollow cathode Nano Thruster used for LEO orbit performance optimisation of the experiments with Hall Thrusters: high voltage power supply S. Gabriel raising Halo thruster on-ground chamber effects on for Power Processing Unit 11.15 D. Krejci S. Masillo measurements and extrapolation Q. Kang to in-flight situation P. Sarrailh

A781 A895 A858 A464 A One-Dimensional model for LISA Colloid Microthruster Thruster Plume and Spacecraft Development of compact Hollow Cathode Orifice lifetime Technology Development Plan Interaction Analysis by 3D high efficiency RF prediction and Progress Electrostatic Code for 4.5-kW- generator for inductive 11.30 F. Bosi J. Ziemer Class Hall Thruster coupled plasma sources T. Muranaka A. Surminskii

A473 Wednesday Parallel codes using particles decomposition and view factor model methods for the particle in cell-Monte Carlo collision 11.45 (PIC-MCC) simulation on cylinder hall thruster R. Pan

Lunch Break 12.00

Plenary Lecture → see page 10 Audimax The Role of EP in Leo Chaired by M. Walker / R. Spears 13.30

1st Chair F. Bosi 1st Chair D. Krejci 1st Chair T. Misuri 1st Chair P. Peterson 1st Chair M. Smirnova 1st Chair M. Micci 1st Chair T. Schönherr 1st Chair Y. Yamakawa 2nd Chair – 2nd Chair L. Massotti 2nd Chair A. Mishra 2nd Chair L. Wei 2nd Chair V. Kozhevnikov 2nd Chair J. Skalden 2nd Chair E. Ahedo 2nd Chair –

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

15.00 with LaB6 emitter tion with spacecraft body A. Markov R. Kawashima mode for 3-grid system ion the PIC-DEM Method inductive pulsed plasma Acceleration Method L. Garrigues M. Villemant thruster L. Brieda thruster T. Furukawa Y. Jia X. Li 50 IEPC19 Programme Wednesday 18 51

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

HS6 SR5 SR6 SR2 HS5 SR4 HS3 HS2

A865 A317 A660 A648 A680 A837 A646 A537 Comparisons between Particle Uncertainty Quantification of I2HET: Development of an Multiscale Hybrid Modeling of Surface Modification of Pyro- Numerical Rebuilding of Very Low Operation and Performance of a An Experimental Study of Thrust Simulation using IAT Growth Electrospray Thruster Array Iodine-Fed Hall Effect Thruster Unconventional Hall Thrusters lytic-Graphite Grids for an Ion Power Arcjet Thruster VELARC Fully-Integrated ion Electrospray Dependence on Magnetic Field in Model and Plume Measurements Lifetime M. M. Saravia M. Laterza thruster in Test Facilities at IRS and Propulsion System an Electrodeless Inductive Plasma 15.15 of LaB6 Hollow Cathode B. Jorns Y. Matsunaga ESA-ESTEC B. Kristinsson Accelerator K. Kubota P. P. Upadhyay A. Tatsuno

A874 A526 A838 A281 A722 A562 A742 A596 Fluid model of a Hollow Cathode Colloid Thruster Plume Simula- Simulation of an Adaptable Hall Plasma Simulations for the Uncertainty Quantification of A Chemically Augmented Arcjet Direct Inertial Electrostatic Development and Character- discharge tions Using a Particle-Particle Thruster Assessment of Pole Erosion in the Modeled Electron Backstreaming Thruster with Exotic Propellants Confinement Propulsion at Low ization of the Helicon Plasma X. Chen Model N. Proulx Magnetically Shielded Miniature Failure for the NEXT Ion Thruster M. Tsuchiya Power Levels Thruster Prototype HPT-03 15.30 J. Wang Hall Thruster (MaSMi) J. Yim M. Winter J. Navarro-Cavallé A. Lopez Ortega

A153 A530 A902 A364 A907 A703 A761 A647 Development of Low-Volt- Effect of Aprotic + Protic Performance, Plume, Stability, Particle-In-cell / fluid simulations Modeling Ion Optics Erosion in Effect of adding water to Experimental demonstration Optimization of electrothermal age-Driven Propellantless Mixtures on Electrospray Droplet and Wear Characterization of of a Hall effect thruster account- the NEXT Ion Thruster Using the propellant of a DME arcjet of thrust vectoring magnetic microwave plasma thruster for Cathodes with High-Current Fragmentation Three Alternate Magnetic Field ing for plasma wall interactions CEX2D and CEX3D Codes thruster nozzle with multi-axis thrust nanosatellites

15.45 Density Based on Graphene-Ox- D. Levin Topologies in the Hall Effect W. Villafana J. Polk T. Tachibana measurement system S. Ivanov ide-Semiconductor Structure Rocket with Magnetic Shielding M. Edamoto R. Furuya H. Kamhawi

A214 A830 A637 A478 A855 Radio Frequency Microdischarge Development of an Electrospray Characterisation and The Sputtering Mechanism of Performance improvement of a Neutralizer Source Model for Kinetic Plume Performance Comparison of a Keeper Electrode in Hall Thruster magnetic nozzle helicon plasma F. Filleul Modeling Low-Power Hall-Effect Thruster J. Chen thruster E. Petro and an Advanced Cusp Field K. Takahashi 16.00 Thruster with Multiple Noble Gases M. Vaupel Wednesday

A565 A752 A867 Numerical simulation of Preliminary Evaluation of Cubesat Test Platform for electrospray thruster extraction Anode-Layer-Type Hall Thruster miniaturized electric propulsion for highly conductive propellants Performance Using Pulsating system verification campaign 16.15 H. Huh Boost Chopper Circuit F. Stesina K. Nagamine

A559 A563 A815 Study on Performance of Ionic Impact on Performance and Enabling High-Energy Missions Liquid Electrospray Thruster Erosion in Hall Thruster using with Nanosatellites by Using in Atmosphere and Vacuum Argon and Xenon propellant Ablative Pulsed Plasma Thrusters 16.30 Environment S. Yokota P. Gessini Y. Guo K. Shimamura

A788 A920 High-Speed Transient Character- The operation of a low-power ization of the Busek BET-300-P cylindrical Hall thruster with zinc

16.45 Electrospray Thruster as the propellant D. Courtney C. Ryan

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

Session End → Gala Dinner beginning 18:30 THURSDAY 54 IEPC19 Programme Thursday 19 55

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

HS6 SR4 SR6 SR2 HS5 SR3 HS3 HS2

1st Chair I. Mikellides 1st Chair J. Trescott 1st Chair C. Boniface 1st Chair R. Heidemann 1st Chair S. Gabriel 1st Chair G. Herdrich 1st Chair M. Merino 1st Chair S. Peterschmitt 2nd Chair X. Chen 2nd Chair K. Dannenmayer 2nd Chair I. Funaki 2nd Chair T. Hallouin 2nd Chair C. Altmann 2nd Chair A. Kitaeva 2nd Chair – 2nd Chair M. Mooney

A249 A592 A793 A487 A287 A493 A164 A188 Comparison of transient behavior The Ariane Group Electric Life Estimation of Hall Thrusters Oscillation analysis in Hall Non-intrusive measurements of Magnetic Field and Current Evaluation of anomalous resistiv- Comparison of waveguide-cou- in a 20 A hollow cathode in a 9 Propulsion Program 2019-2020 using Multi Spectral Imaging thrusters with 2D (axial-azimuth- microwave ion thruster by two Density Probe for Steady State ity in a low power magnetic pled and coaxial-coupled ECR kW Hall thruster and a stand- H. Leiter H. Gole al) Particle-In-Cell simulations photon absorption LIF and laser AF-MPD Thrusters nozzle magnetic-nozzle thruster using a 09:00 alone configuration T. Charoy Thomson scattering A. Behnke S. Hepner thrust balance M. Georgin R. Tsukizaki S. Peterschmitt

A430 A926 A408 A501 A337 A551 A199 A219 Mechanism Analysis of Cathode Overview of Busek EP Thrusters Terahertz Time-Domain Enhancing Hall Effect Thruster Estimation of Erosion Rate for Simultaneous Measurement of Experimental Validation and Optimization of a Low Power ECR Low Frequency Oscillation V. Hruby Spectroscopy as an Electric Simulations with Deep Recurrent Surface Material on HAYABUSA2 Cathode Surface Temperature Performance Measurements of Thruster Using Pulsed Power and Z. Ning Propulsion Plasma Diagnostic Networks by Measurement of Backflow Ions Distribution and Plasma Spatial an ECR Thruster Operating on Frequency Mixing Techniques

09.15 N. Brown P. Shaw from 10-cm-class Ion Thruster Distribution in Self-Field MPD Multiple Propellants B. Wachs T. Muranaka Thruster R. Moloney S. Tauchi

A604 A600 A861 A732 A348 A310 A261 A267 Applicability of electride Electric Propulsion Develop- Application of Helium Line Data-Driven Modeling for A novel optical line-ratio method The Experimental Performances The SpaceDrive Project – Development of the hall effect materials for hollow cathodes ments at Rafael in 2019 Intensity Ratio Spectroscopy Nonlinear Dynamics of Phys- for measuring the electron of the 100kW MPD Thruster with EMDrive Thrust Measurements hollow cathode thruster M. Reitemeyer D. Lev to Xenon plasma in Penning ical Phenomena in Hall Effect parameters in the discharge Applied Magnetic Field and Analysis L. Chenguang 09.30 discharge Thrusters chamber of xenon ion thrusters Y. Cong M. Tajmar H. Sekine K. Hara X. Zhu

A929 A516 A579 A396 A759 A262 A363 Additively Manufactured Hollow Hall Thruster Plume Measure- Analysis of the plasma discharge Optical plasma diagnostics for Characterization and Improve- The SpaceDrive Project – Over- Diagnostics and testing Cathode Keepers with Integral ments of Time Resolved Ion in a Hall thruster via a hybrid 2D radio-frequency ion thrusters ment of Thrust Balance for view of Revolutionary Propulsion facilities for ionic liquid electro- Radiation Shielding Energy code B. Nauschütt High Power Applied Field MPD Efforts at TU Dresden spray thrusters at the Air Force 09.45 M. S. McDonald M. Baird P. Fajardo Thrusters M. Tajmar Research Laboratory G. Herdrich D. Eckhardt

A845 A308 A613 A503 A314 A271 A417 Total Sputter Yield Character- Electron cross-field transport Boundary conditions for a Two-Photon Laser-Induced Cathode Ablation Performance of Plasma Jet Pack (PJP) REGULUS: Iodine Fed Plasma ization of Various Spacecraft mechanism observed under the two-dimensional direct kinetic Fluorescence Diagnostics of a Applied-Field Magnetoplasma- Technology Propulsion System for Small Materials azimuthally inhomogeneous simulation of a Hall thruster Radiofrequency Ion Thruster: dynamic A. Blanchet Satellites

10.00 J. A. Young neutral supply in a Hall thruster A. Raisanen Measurements in Xenon and G. Wang M. Magarotto J. Bak Krypton C. Eichhorn

A155 A449 A619 A167 A585 A290 A498 Thursday Onset criteria for the plume On-board Plasma Plume Operation of a Low Power Near Field Probe Measurements Current Advances in Optimiza- Characterisation of a Rotational XMET: Design and early testing of mode oscillation in hollow Diagnostics for ETS-9 All-electric Hall Thruster with a Shielded in the Plume of a NEXT Ion tion of Operative Regimes of Thrust Balance for Propellantless a xenon microwave electrother- cathodes Satellite Magnetically Configuration Thruster Steady State Applied Field MPD Propulsion Concepts Utilizing mal thruster

10.15 M. Georgin K. Kinefuchi L. Garrigues N. Arthur Thrusters Magnetic Levitation with D. Staab A. Boxberger Superconductors O. Neunzig

A667 A252 A642 A738 A401 A292 A638 The neutral gas properties in Significant ion acceleration of Influence of Magnetic Field Determination of the Beam Anode Power Deposition in Influence of cathode grid dimen- Analytical plasma modelling orifice hollow cathode before Xe ions outside the discharge Strength on Narrow Channel Hall Divergence of a Gridded Ion an AF-MPDT with Two Unique sion on discharge characteristics and design upgrade for an ECR its ignition channel in cylindrical Hall Thruster Discharge Operating at Thruster Using the AEPD Platform Magnetic Field of IEC thruster thruster operating on water and

10.30 Y. Jia thruster plasmas observed by Very Low Power F. Scholze P. Wu Y.-A. Chan ammonia propellants laser induced fluorescence I. Kronhaus E.R. Azevedo G. Doh

A246 A720 A777 A588 A333 A875 Hall Thruster Near-Field Plume Numerical studies of the ExB Planar probe array for bidimen- Experimental study of the High-Specific-Impulse Operation H2020 MINOTOR: Magnetic Characterization Through Optical electron drift instability in Hall sional mapping of the ion flux discharge characteristic in in Diverging Magnetic Field Nozzle Electron Cyclotron Emission Spectroscopy thrusters profile of a miniaturized ion AF-MPDT ignition Electrostatic Thrusters with Resonance Thruster 10.45 M. Nakles F. Taccogna thruster Y. Wang Argon Propellant D. Packan L. Habl D. Ichihara 56 IEPC19 Programme Thursday 19 57

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

HS6 SR4 SR6 SR2 HS5 SR3 HS3 HS2

A387 A437 A145 A382 A941 Study of two different discharge 3D simulation of rotating spoke in Radio-frequency biasing of ion Metallic Ion Thruster using Mag- Development of the Xenon modes in Hall thruster a wall-less Hall thruster thruster grids netron E-Beam mombardment Cold Gas Thruster to Support

11.00 I. Khmelevskoi K. Matyash T. Lafleur K. Chen All-Electric Propulsion Missions I. Johnson

A726 A507 A385 A608 Development of 1D Magneto-stat- A global performance model of Thrust Generation in Electro- XMET: Testing of an Argon/ ic Two-Fluid Plasma Simulation of Gridded Ion Thrusters static-Magnetic-Hybrid Plasma Xenon Microwave Electrothermal

11.15 a Hall Effect Thruster E. Ahedo Thruster Thruster K. Hara A. Sasoh T. Baxter

A475 Design and Performance Test of a RF Plasma Bridge Neutralizer

11.30 D. Spemann 11.45

Lunch Break & Poster Session 12.00

Plenary Lecture → see page 11 Audimax BEPI Colombo – The Mission

14.00 Presented by Neil Wallace / Chaired by Carsten Scharlemann

1st Chair J. Gonzalez del Amo 1st Chair S. Mazouffre 1st Chair N. Yamamoto 1st Chair J. Brophy 1st Chair A. Boxberger 1st Chair M. Winter 1st Chair S. Rojas Mata 2nd Chair N. Wallace 2nd Chair Y. Nakayama 2nd Chair H. Kamhawi 2nd Chair E. Petro 2nd Chair H. Tahara 2nd Chair – 2nd Chair T. Furukawa

A824 A841 A733 A175 A195 A488 A467 BepiColombo – Non-intrusive Characterization Coupling Non-Maxwellian View Design and Experimental Study of A Novel Laser Ablation Magneto- Inductive Plasma Thruster (IPT) Performance Analysis of the A mission overview of the Wear of the HERMeS Factor Model to Octree Based an Miniature Ion Thruster plasmadynamic Thruster for an Atmosphere-Breathing Capacitively Coupled Radio

N. Wallace Thruster Using Optical Emission Particle VDF Compression for J. X. Ren Y. Zhang Electric Propulsion System: Frequency Thruster Thursday

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

A305 A932 A880 A238 A313 A500 A577 BepiColombo - Solar Electric Internal Probe Studies of a Low Particle-In-Cell model of the Preparation of Space Experiment Development of High Power Review of Dualmode/Multimode Proposal and Performance Propulsion System Operations Voltage Hall Thruster dynamic of the electrons between with Electric Propulsion System Magnetoplasmadynamic Space Propulsion Evaluation of Microwave-Driven for the Transit to Mercury J. L. Ross the two walls of Hall thrusters Based on Radio-Frequency Ion Thrusters in BICE and Beihang C. Lyne In-Tube Accelerator Concept

15.15 C. Steiger including realistic secondary Thruster aboard the International University M. Takahashi electron emission data Space Station Y. Li M. Villemant R. Akhmetzhanov 58 IEPC19 Programme Thursday 19 59

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

HS6 SR4 SR6 SR2 HS5 SR3 HS3 HS2

A606 A384 A718 A239 A542 A552 A594 BepiColombo – The Mercury Incoherent Thomson scattering Investigation of cross-field Atmospheric Ramjet Thrust Unit Applied-Field MPD Thruster with Interaction of Ultraviolet Indirect electrothermal Transfer Module investigations of a low-power electron transport in a 100-W on the Base of High-frequency High Current Heater-less Hollow Light-emitting Diodes and Solid acceleration of a cold gas jet H. Gray Hall thruster in standard and class Hall Thruster using a full Ion Thruster Cathode Polymers for Micropropulsion through interaction of an arcjet

15.30 magnetically-shielded configu- particle-in-cell simulation V. Kozhevnikov J. Yamasaki Applications exhaust flow for space propulsion rations S. Cho H. Horisawa applications B. Vincent Y. Arai

A494 A617 A582 A240 A872 A605 A610 BepiColombo – MTM and MEPS Characterization and perfor- Experimental characterization Characteristics of Radio-Fre- Development of a 10-30 kW Hybrid Electric Propulsion Informing the design of pure-ion Integration and Verification mance measurements of 40 and modeling of ID-HALL, a quency Ion Thruster with an Augmented Field MPD Thruster System based on Water electrospray thrusters via K. Kempkens W-class and 100 W-class Hall double-stage Hall thruster with Additional Magnetic Field in the at SITAEL Electrolysis simulation of the leaky-dielectric 15.45 thrusters an inductive ionization stage Ionization Area A. Kitaeva N. Harmansa model with charge evaporation T. Hallouin Á. Martín Ortega V. Kozhevnikov X. Gallud Cidoncha

A586 A528 A447 A339 A450 A621 A643 BepiColombo - Solar Electric Development Efforts on a Laser Performance Evaluation of a Ring Cusp Ion Thruster IT-200PM Performance of Applied Field Advanced Cusp Field Thruster Physics and performance of the Propulsion System Test and Thomson Scattering Diagnostic 100-W Class Hall Thruster A. Lovtsov MPD Thruster with Various with a 3D-printed discharge Alternative Low Power Hybrid Qualification Approach for Electric Propulsion Applica- H. Watanabe Propellants channel - Performance with Ion Engine (ALPHIE) for space 16.00 S. Clark tions S. Ide Iodine and Xenon propulsion T. Matlock M. Vaupel J. González

A615 A598 A816 A574 A870 A692 A775 BepiColombo – MEPS Experimental Study on the Scaling of spoke rotation fre- Test Campaign on the novel Plasma Plume Characteristics of 13kW Advanced Electric Propul- Azimuthal Induced Current commissioning activities and Influence of Magnetic Field on quency within an ExB Discharge Variable Isp Radio Frequency Mini Cluster Operation of Self-Field sion Flight System Development Formation and Ion Acceleration T6 ion thruster performance the Performance of Low-power A. Powis Ion Engine Magnetoplasmadynamic and Qualification in an Inductive Radiofrequency 16.15 during early mission operations Hall Thrusters M. Smirnova Thruster J. Jackson Plasma Thruster R. Lewis X. Yi Y. Murayama H. Sekine

A298 A352 A797 A329 A712 A829 Pole Erosion Measurements for Neutral gas instabilities in Hall Exprimental studies on the effect Research on the 500kW The SpaceDrive Project – Two-dimensional Full the Development Model of the thrusters, Part I: Measurements of the magnetic field and the Class Superconducting Progress in the Investigation Particle-In-Cell Simulation of Magnetically Shielded Miniature E. Dale electrical potential inside the Strong Magnetic Field High of the Mach-Effect-Thruster Magnetic Sails in Formation Flight

16.30 Hall Thruster (MaSMi-DM) water ion thruster Power Magnetoplasmadynamic Experiment A. Wada R. Lobbia Y. Ataka Thruster Technology M. Monette C. Zhou

A432 A806 A801 A774 A903 Driving Low Frequency Oscilla- A Nouvelle Neutralization Business Cases and System Development of a deployable An experimental revisit of plasma tions in Hall Thruster Concept for RIT-µX Miniaturized Architecture for Superconduc- vacuum arc thruster system for phenomena on Helicon Plasma Y. Raitses Radio Frequency Ion Thruster tor-based Applied Field Magneto the post-mission disposal of Thrusters Thursday 16.45 Systems Plasma Dynamic Thrusters micro/nano satellites J. Navarro Cavalle H. Leiter M. La Rosa Betancourt M. Kim 60 IEPC19 Programme Thursday 19 61

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

HS6 SR4 SR6 SR2 HS5 SR3 HS3 HS2

A209 A354 A808 A886 A365 Hall Thruster Erosion Meas- Neutral gas instabilities in Hall The RIT 2X High Performance Ion Development Roadmap of RF Power - Plasma Coupling urement by Time-Resolved thrusters, Part II: Theory Thruster System Qualification SITAEL’s RAM-EP System Experimental Results in a Helicon

17.00 Cavity-Ring Down Spectroscopy E. Dale Program T. Andreussi Plasma Thruster Prototype Y. Egawa M. Berger V. Gómez

A332 A632 A842 A293 A940 Numerical simulation and Influence of double-stage Charge State Thrust Correction Back-vacuum Retarding Poten- A thruster using magnetic experimental research on low operation on breathing oscilla- Factor for NEXT: DART Mission tial Analyzer for Investigation of reconnection to create a high- power Hall thruster with long life tions and rotating spokes in the IEC plasma properties speed plasma jet

17.15 M. Crofton Y. Ding ID-HALL thruster Y.-A. Chan S. Bathgate A. Guglielmi

A749 A433 A844 A434 Prediction of liner erosion and Use of electrostatic probes for Deposition Rate Measurements in Beam Plasma Expansion of a life estimation of Stationary characterization of the electron NEXT Ion Engine Plume for DART Helicon Plasma Source Plasma Thrusters using Machine cross-field current in ExB plasmas Mission Z. Zhang 17.30 Learning Y. Raitses J. Young A. Mishra

A323 A853 A448 Experimental study on the effect NEXT Single String Integration Modeling and Optical Diagnos- of propellant asymmetrical Tests In Support of the Double tics of Iodine Fed Helicon Type distribution on plasma potential Asteroid Redirection Test Mission Thrusters by a Detailed Global

17.45 distribution in a Hall effect R. Thomas Model (DGM) thruster K. Katsonis M. Ding

A859 A682 Experimental Characterization of A Detailed Global Model for the Microwave-Discharge Water Modeling and Optical Diagnos- Ion Thruster for CubeSats tics of Low Power Propulsion 18.00 Y. Nakagawa Devices Fed by CO2 C. Berenguer

Session End 18.15 Thursday FRIDAY 64 IEPC19 Programme Friday 20 65

Hall Thrusters 1 Propellant Storage Mission Diagnostic Hall Thrusters 2 / Feed Systems

HS6 SR5 HS2 HS3 HS5

1st Chair T. Andreussi 1st Chair P. Barbier 1st Chair D. Oh 1st Chair T. Trottenberg 1st Chair T. Lafleur 2nd Chair Ya. Hu 2nd Chair H. Liu 2nd Chair N. Wallace 2nd Chair J. Laube 2nd Chair L. Garrigues

A665 A601 A192 A374 A545 Plasma fluctuations measurements in a Hall Innovative Xenon/Krypton FMS (Feed Man- Development of the Psyche Mission for NASA's Three-dimensional Vector Measurement Fluid modeling of gradient-drift turbulence Thruster agement System) for Electric Propulsion Discovery Program of EP Propellant Flow within a Vacuum and transport in ExB plasmas

09:00 N. Yamamoto P. Barbier D. Oh Chamber A. Smolyakov Y. Nakayama

A687 A400 A244 A517 A691 Axial-azimuthal high-frequency instability Development of Porous-Metal-Restrictor Electric Propulsion for the Psyche Mission In-situ microscopy of ion-induced erosion of New insights into electron transport due to modes in a Hall thruster fluid model Based Xenon Flow Control Modules S. Snyder plasma-facing surfaces azimuthal drift in a Hall effect thruster

09.15 E. Bello-Benítez G. Hang A. Ottaviano K. Hara

A454 A654 A258 A569 Effect of magnetic field configuration on Sitael HT100 Missions: uHETSAt and PLATiNO Thrust measurements using plasma pressure Assessment of the thermodynamic and discharge characteristics in permanent T. Misuri measurements in the plume: a feasibility fluid approximations for electrons in plasma

09.30 magnet thrusters with cusped field study thruster plumes S. Liang P.-Q. Elias Yu. Hu

A593 A138 A887 A304 Simulation of radial electron dynamics in a Status Update on the Electric Propulsion Recent Advances in Plasma Diagnostics at Characteristic Transient Phenomena of Hall Hall effect thruster Subsystem of TURKSAT6A Communication IRS Effect Thrusters

09.45 A. Domínguez-Vazquez Satellite G. Herdrich A. Komarov B. C. Aydin

A479 A927 A345 A758 Predicting secondary electron emission rate Mars Sample Return - Earth Return Orbiter: Development of a Flight Electric Propulsion Plasma instabilities in cross-field configura- in Hall Effect Thrusters ESAs next Interplanetary Electric Propulsion Diagnostic Package (EPDP) for EP Satellite tion: an analysis of the relevance of different

10.00 A. Tavant Mission Concept Platforms modes for electron transport O. Sutherland T. Trottenberg S. Tsikata

A514 A411 A115 A843 Enhancing thrust by ion-neutral collisions Electric Propulsion Characterisation for a Use of Real-Time Spectrum Analysis for EMI Experimental Correlation between and by oscillating EM fields Stand-Alone Mars CubeSat Characterization of a SAFRAN Hall Thruster Anomalous Electron Collision Frequency and

10.15 A. Fruchtman K. V. Mani W. Tighe Plasma Turbulence in a Hall Effect Thruster Z. Brown

A523 Effects of large scale structures on anomalous transport in PIC simulations of Electron Cyclotron Drift Instability in Hall thrusters 10.30 A. Smolyakov

A543 Towards Predictive Kinetic Simulations of Plasma Thrusters Friday

10.45 I. Kaganovich

Briefing Technical Tour Audimax 11.00 66 IEPC19 Programme Information 67

Calling to and from Austria Post Office Full Papers Health Care

International country code for Austria +43 The closest post office is a 10-15 minute walk located in Full Papers will be published online on our website. In case you need assistance for urgent medical issues or the local city code for Vienna is 1 the Alserstraße: “Postfiliale und Bawag PSK”, Alserstraße any injuries please contact either the registration desk, National calls: 0 + city code + number 31, Mon-Fri 08:00-18:00. Take tram no 43 or 44 for 2 sta- Badges a member of the IEPC 2019 staff, or call: International calls: tions from Schottentor. +43 664 602 77 17 630 00 + country code + city code + number Admission to the conference venue is possible with a USA calls: 001 + areacode + number Public Transportation valid name badge only. Badges must be used throughout Insurance the entire conference and at the official social events. Currency / ATM This is the most economical way to travel in Vienna – REMEMBER your badge even for excursions or the confer- The IEPC 2019 cannot accept liability for personal injuries aside from walking. You can purchase tickets online (www. ence dinner. In case of loss you can obtain a replacement at sustained, or for loss or damage of personal belongings ei- The currency used in Austria is the Euro (€). You may ex- wienerlinien.at) or use one of the vending machines at the registration desk at a fee of € 30,00. Return of badges ther during or as a result of the meeting. Please check the change foreign currencies at one of the bank institutes Schottentor. You can find them downstairs on the way to the is highly appreciated (in the box located at the registration validity of your personal insurance. next to the university building (See Area Map) Volksbank subway station of the U2 (violet line), just before entering desk). (Schottengasse 1, Mon-Fri 08:00-12:30); UniCredit Bank the escalator down to the platforms. Do not forget to vali- Language Austria (Schottengasse 11, 24h service foyer); Oberbank date your ticket on one of the blue validation machines. The Coffee and Lunch Breaks (Schottengasse 2, Mon-Fri 08:00-12:30). There are also public transportation organisation (Wiener Linien) also pro- The official meeting language is English. cash machines/ATMs (in Austria called “bankomat”) availa- vides special tourist tickets called Vienna Card, which com- Food, hot and cold beverages will be served during the con- ble at these locations. In addition, there is one ATM available bine public transport with reduced fees to the most popular ference day and the lunch breaks free of charge. Lunch is Photographer inside the university building in the corridor on the ground touristic sites in Vienna. available for all participants at two places in the exhibition level leading to the Audimax lecture hall. area (under the arcades). The entire conference will be documented by a team of Taxi professional photographers. Electricity Special dietary requirements have been communicated to The closest taxi stands are located in the Schottengasse the conference caterer. Please inform the catering person- Registration Desk The electric voltage in Austria is 230 V AC (at 50Hz). You (next to the Schottentor) or on Rooseveltplatz (opposite of nel, they will help you. Remember to wear your badge during can use your equipment, if the outlet voltage in your country the hotel “Regina”). You can also call a taxi (+43 1 40 100 lunch and coffee breaks. Sunday 15th 16:00 – 18:00 ranges between 220 and 240 V, otherwise you have to use or +43 1 31 300). Uber is available in Vienna as well. For Monday 16th 08:00 – 17:00 an adapter (100-240 V 50/60Hz). You have to use 2-pin ordering taxi to the airport we recommend to use one of the Wardrobe Tuesday 17th 08:00 – 10:00 type C or type F plugs for Austrian sockets. airport taxi shuttle services (>1 day in advance) at a fixed Wednesday 18th 08:00 – 15:00 prize (€ 30-35), e.g. www.airportdriver.at A wardrobe on the lower level is available for storage of Thursday 19th 08:00 – 17:00 Emergency Calls clothes and luggage. It will be open during the session Friday 20th 08:00 – 12:00 Health Service / Hospital times. Please note that the room will be attended during Fire brigade: 122, Police: 133, Ambulance: 144, these times, but storage is at your own risk with respect Smoking at the IEPC 2019 European emergency call: 112 If you need urgent medical care the closest hospital is the to loss and damage. “Allgemeine Krankenhaus (AKH) Wien” (www.akhwien.at), Smoking is not allowed in the entire building of the Parking 1090 Wien, Währinger Gürtel 18-20. Exhibition Opening Hours University of Vienna, with the exception of the Arcaded Courtyard. Thank you for understanding. Parking is very restricted in Vienna, in particular in the Supermarkets Monday 16th 09:00 – 17:00 area of the city centre. You have to use pre-paid tickets Tuesday 17th 09:00 – 11:00 WIFI (“Kurzparkscheine”), which are available in four colours The nearest supermarkets within 5-6 minutes walking dis- Wednesday 18th 09:00 – 17:00 (red = 1/2 hour, € 1,05; blue = 1 h, € 2,10; green = 1 ½ h, tance from the IEPC 2019 site are: BILLA (Universitätsstraße Thursday 19th 09:00 – 17:00 Free WIFI internet access is available throughout the en- € 3,15; and yellow = 2 h, € 4,20). These tickets can be 6-8, Mon-Fri 7:40-20:00), and SPAR Gourmet (Schotten- Friday 20th 09:00 – 13:00 tire venue. You can find the access code/voucher on the purchased at any newspaper kiosk (“Trafik”). The clos- gasse 7, Mon-Fri 07:30-20:00). reverse side of your name badge. est “Trafik” to the IEPC 2019 venue is located directly at Schottentor, next to the tram station of lines 43, 44, D, 71. Weather Parking with these tickets is limited to maximum 2 hours. You can also use equivalent electronic tickets by using an In September there is significant continental influence. The app when registering your car on www.handyparken.at. average temperature is 16°C in the morning, 22°C during If you want to park for longer you have to use one of the the day and 20°C in the evenings. The temperatures during car parks. The closest is the “WIPARK Votivpark-Garage” the day can vary between a minimum of 6°C and a maximum in the Universitätsstraße (24 hours open, € 4,30 per hour, of 31°C. While the rain ranges between 26mm and 89mm € 43,-- per day) per month, sunshinehours of up to 260 are possible. 68 IEPC19 Programme

Index of Sponsors and Supporters

AAC FOTEC Forschungs- und Technologietransfer GmbH www.aac-research.at www.fotec.at

AC2T Huazhong University of Science & Technology www.ac2t.at english.hust.edu.cn

Aerojet Rocketdyne Hot Head Music Club www.rocket.com www.hotheadmusicclub.com

Ariane Group Luftballonia www.ariane.group www.luftballonia.at

BUSEK Space Propulsion and Systems Ortner4Dance busek.com www.ortner4dance.com

CEST RAFAEL Advanced Defense Systems LTD. www.cest.at www.rafael.co.il

COBHAM RUAG www.cobham.com/mission-systems www.ruag.com

COLUMBUS Ihr Reisebüro GmbH & Co.KG. SAFRAN www.columbus-dmc.com www.safran-group.com

DDSG Blue Danube Schiffahrt GmbH SITAEL www.ddsg-blue-danube.at www.sitael.com

DISS The Linde Group www.donau-uni.ac.at/de/universitaet/fakultaeten/ www.the-linde-group.com bildung-kunst-architektur/departments/ integrierte-sensorsysteme The Aerospace Corporation aerospace.org ELIAS Music www.eliasmusic.at TUBITAK www.tubitak.gov.tr ENPULSION www.enpulsion.com Universität Wien www.univie.ac.at ERPS – Electric Rocket Propulsion Society erps.spacegrant.org VACCO www.vacco.com Fachhochschule Wiener Neustadt www.fhwn.ac.at Wiener Neustädter Stadtwerke und Kommunal Service GmbH FFG www.wnsks-reisebuero.at www.ffg.at iepc2019.univie.ac.at