BEGIN:VCALENDAR PRODID:-//Microsoft Corporation//Outlook 16.0 MIMEDIR//EN VERSION:2.0 METHOD:PUBLISH X-CALSTART:20231001T160000Z X-CALEND:20231006T120000Z X-WR-RELCALID:{0000002E-82DB-96FB-B151-E68C6B74ADAE} X-WR-CALNAME:ESPC2023: Sessions Power calendar BEGIN:VTIMEZONE TZID:W. Europe Standard Time BEGIN:STANDARD DTSTART:16011028T030000 RRULE:FREQ=YEARLY;BYDAY=-1SU;BYMONTH=10 TZOFFSETFROM:+0200 TZOFFSETTO:+0100 END:STANDARD BEGIN:DAYLIGHT DTSTART:16010325T020000 RRULE:FREQ=YEARLY;BYDAY=-1SU;BYMONTH=3 TZOFFSETFROM:+0100 TZOFFSETTO:+0200 END:DAYLIGHT END:VTIMEZONE BEGIN:VEVENT CATEGORIES:Yellow Category CLASS:PUBLIC CREATED:20230616T121549Z DESCRIPTION:Sponsored by Azur Space.\nWhere: https://goo.gl/maps/9B7BoiqbZq WCEC3W8\n DTEND;TZID="W. Europe Standard Time":20231005T203000 DTSTAMP:20230929T062735Z DTSTART;TZID="W. Europe Standard Time":20231005T193000 LAST-MODIFIED:20230927T141935Z LOCATION:Hotel Meliá Alicante PRIORITY:5 SEQUENCE:0 SUMMARY;LANGUAGE=en-gb:Cocktail before Gala dinner (sponsored by Azur Space ) TRANSP:OPAQUE UID:040000008200E00074C5B7101A82E00800000000E02EAFE25BA0D901000000000000000 01000000036973F0BAD5D60439BF6B88E913B7B14 X-ALT-DESC;FMTTYPE=text/html:< !--[if gte mso 9]>\n\nClean\nClean\n\n\n\n\n\nfalse\nfalse\nfalse \n\nEN-G B\nX-NONE\nX-NONE\n\n\n\n\n\n\n\n\n\n\n\n\n\n< m:brkBin m:val="before"/>\n\n\n\n\n\ n\n\n\n\n \n

Sponsored by Azur Space.

Where: https://goo.gl/maps/9B7BoiqbZqWCEC3W8

< /body> X-MICROSOFT-CDO-BUSYSTATUS:BUSY X-MICROSOFT-CDO-IMPORTANCE:1 X-MICROSOFT-DISALLOW-COUNTER:FALSE X-MS-OLK-AUTOFILLLOCATION:FALSE X-MS-OLK-CONFTYPE:0 BEGIN:VALARM TRIGGER:-PT15M ACTION:DISPLAY DESCRIPTION:Reminder END:VALARM END:VEVENT BEGIN:VEVENT CATEGORIES:Yellow Category CLASS:PUBLIC CREATED:20230616T121549Z DESCRIPTION:Music sponsored by SAFT.\nWhere: https://goo.gl/maps/9B7BoiqbZq WCEC3W8\n DTEND;TZID="W. Europe Standard Time":20231006T000000 DTSTAMP:20230929T062735Z DTSTART;TZID="W. Europe Standard Time":20231005T203000 LAST-MODIFIED:20230927T142035Z LOCATION:Hotel Meliá Alicante PRIORITY:5 SEQUENCE:0 SUMMARY;LANGUAGE=en-gb:Gala dinner: Hotel Meliá Alicante (music sponsored by SAFT) TRANSP:OPAQUE UID:040000008200E00074C5B7101A82E0080000000020E5C6985BA0D901000000000000000 0100000000B67405A68D09243B1795E135120BCFA X-ALT-DESC;FMTTYPE=text/html:< !--[if gte mso 9]>\n\nClean\nClean\n\n\n\n\n\nfalse\nfalse\nfalse \n\nEN-G B\nX-NONE\nX-NONE\n\n\n\n\n\n\n\n\n\n\n\n\n\n< m:brkBin m:val="before"/>\n\n\n\n\n\ n\n\n\n\n \n

Music sponsored by SAFT.

Where: https://goo.gl/maps/9B7BoiqbZqWCEC3W8

< /body> X-MICROSOFT-CDO-BUSYSTATUS:BUSY X-MICROSOFT-CDO-IMPORTANCE:1 X-MICROSOFT-DISALLOW-COUNTER:FALSE X-MS-OLK-AUTOFILLLOCATION:FALSE X-MS-OLK-CONFTYPE:0 BEGIN:VALARM TRIGGER:-PT15M ACTION:DISPLAY DESCRIPTION:Reminder END:VALARM END:VEVENT BEGIN:VEVENT CATEGORIES:Yellow Category CLASS:PUBLIC CREATED:20230616T121549Z DESCRIPTION: \n DTEND;TZID="W. Europe Standard Time":20231002T202000 DTSTAMP:20230929T062735Z DTSTART;TZID="W. Europe Standard Time":20231002T182000 LAST-MODIFIED:20230927T131702Z LOCATION:Exhibition area PRIORITY:5 SEQUENCE:0 SUMMARY;LANGUAGE=en-gb:Cocktail: Exhibition opening TRANSP:OPAQUE UID:040000008200E00074C5B7101A82E00800000000801916065BA0D901000000000000000 0100000001C6AC4043D148749896A4AA08CE449A4 X-ALT-DESC;FMTTYPE=text/html:< !--[if gte mso 9]>\n\n\n\n\n\n\nfalse\nfalse\nfalse\n\nEN-GB\nX-NONE\nX-NONE\n\n\n\n\n\n\n\n\n\n\n\n\n\n\n\n\n\n\n\n\n\n\n\n\n

 \ ;

X-MICROSOFT-CDO-BUSYSTATUS:BUSY X-MICROSOFT-CDO-IMPORTANCE:1 X-MICROSOFT-DISALLOW-COUNTER:FALSE X-MS-OLK-AUTOFILLLOCATION:FALSE X-MS-OLK-CONFTYPE:0 BEGIN:VALARM TRIGGER:-PT15M ACTION:DISPLAY DESCRIPTION:Reminder END:VALARM END:VEVENT BEGIN:VEVENT CATEGORIES:Yellow Category CLASS:PUBLIC CREATED:20230616T121549Z DESCRIPTION:Where: https://goo.gl/maps/GRogaHhkNrFv5cz9A\nhttps://www.huert odelcura.com/en/\n DTEND;TZID="W. Europe Standard Time":20231004T201500 DTSTAMP:20230929T062735Z DTSTART;TZID="W. Europe Standard Time":20231004T181500 LAST-MODIFIED:20230927T135524Z LOCATION:Huerto del Cura Botanic Garden PRIORITY:5 SEQUENCE:0 SUMMARY;LANGUAGE=en-gb:Mid-Conference cocktail (sponsored by Airbus) TRANSP:OPAQUE UID:040000008200E00074C5B7101A82E0080000000000C01A3A5BA0D901000000000000000 010000000908D4B2EC7FE3648B213D077D7691B95 X-ALT-DESC;FMTTYPE=text/html:\n\nClean\nClean\nDocumentE mail\n\n\n\n\n\nfalse\nfalse\nfalse\n\nEN-GB\nX-NONE\nX-NONE\n\n\n\n\n\n\n\n\n\n\n\n\nMicrosoftInternetExplorer4\n\n\n\n\n\ n\n\n\n\n\n\n\n\n

Where: https://goo.gl/maps/GRogaHhkNrFv5cz9A

https ://www.huertodelcura.com/en/

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Please\, register for this event.

 \;

https://atpi.eventsair.com/espc2023/visit-of-elche

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Design and Optimization of Reconfigurable Hig h-Voltage Power Supply with Interlock Function

Power Management

< p class=MsoNormal align=center style='text-align:center'>Smart Battery Modules for distributed electric al power systems

Modular Power Condit ioning and Distribution Unit within the Advanced Data &\; Power Managem ent System

MicroSADA-18 development of one axis solar array drive mechanism for small satellites

HERA EPS Design Challenges

< /td>

High Voltage on PCB study

Fl exible base power and isolation unit for robotic payloads

Accurate Controllable 325W Laser Diode Driver for Optic al Inter-Satellite Links

Evolution of i n-orbit health management strategy for GEO satellite lithium-ion battery

ADS SpE Fr - New Space Electronics for < span class=SpellE>OneSat Avionics

External Battery Charging and Thermal Management for Deep-Space Micro-S atellite: DART &\; LICIACube Missions

Spacecraft Wireless Solar Array Drive As sembly Based on Magnetically Coupled Wireless Transmission Technology

 \;

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 \ ;

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 \ ;

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 \ ;

X-MICROSOFT-CDO-BUSYSTATUS:BUSY X-MICROSOFT-CDO-IMPORTANCE:1 X-MICROSOFT-DISALLOW-COUNTER:FALSE X-MS-OLK-AUTOFILLLOCATION:FALSE X-MS-OLK-CONFTYPE:0 BEGIN:VALARM TRIGGER:-PT15M ACTION:DISPLAY DESCRIPTION:Reminder END:VALARM END:VEVENT BEGIN:VEVENT CATEGORIES:Green Category CLASS:PUBLIC CREATED:20230616T121547Z DESCRIPTION:Historic Session\nHistoric evolution of the Power System for Sp ace application in Europe\nMonday\, 2 October 17:00 -18:20\nAUdiTORIUm\nPr esenters: José A Carrasco (Universidad Miguel Hernández) and Ferdinando Tonicello (ESA)\nThis session is a tribute to the individuals who contribu ted their ingenuity to the different power system technologies and shared their ideas with us through the ESPC. The European space era started with precarious computers and software\, few basic components and not much flig ht heritage and has developed over the years to amazing power system engin eering products\, some of which remain in use today. We hope you will be i nspired by the brilliant minds on stage and by the iconic papers in the bo oklet\, given with the conference kit\, that paved the way for all of us a nd made this conference what it is today.\n \nGuests:\n\nALan Weinberg\n"W e were proud of the fact that our designs were copied by the rest of the w orld and are used even today in most high power Sats as well as the ISS. S ome concepts\, like current-mode control are also used in commercial indus try.”\n \nAlan Weinberg got his first power electronicsexperience at Ple ssey UK designing solid-state standby emergency generators and aircraft Cy cloconverters. Moved to BAe Stevenage and worked on the GEOS and Bluestrea k rocket. \nRecruited to Join ESRO at Estec in 1973 working in the power e lectronics section\, where he supported many projects such as OTS\; ECS\; Meteosat\; Olympus\; Hipparcos\; Hubble Space Telescope and in addition me ntoring Spanish trainees in the art of space circuit design. He left ESA i n 1995 and as a consultant he was involved in many projects\, the most sig nificant being designing the Power System for two prototype spacecraft i.e . the First European GPS Giove-A and Esail Marine Sat. He presently runs a consultancy company.\n________________________________\n\n\nEd Bongers\n “In-orbit short circuits on ECS and the findings of NASA's Long Duration Exposure Facility (LDEF) taught us that both GEO and LEO environment were even more harsh than expected. In-orbit failure investigations on ECS yie lded more knowledge on design and test requirements\, which are still appl ied today.”\n \nAfter studying physics and a research period of 6 years at Leiden University\, EB joined Fokker Space in 1983. His first Solar Arr ay task was technical responsibility for the Eureca solar array PVA and el ectronics and the development of the ARA Mk2 PVA and Thermal Knife HDRS. I n 1991 He became head of solar array engineering at Fokker Space & Systems and project manager of many solar array development projects. After being company head of Technology and Innovation from 2006 till 2014\, his last carrier step has been Senior Expert Solar Arrays within Airbus. In the mea ntime\, he has been leader of the European diode working group and conveno r for the ECSS-E-ST-20-08. His final activity was the design\, development \, and qualification of the recently launched JUICE Solar Array.\nHe retir ed in 2021.\n________________________________\n\n\nAlbert Crausaz\n“As a n anecdote\, at that time in ‘86\, a IRF150 was worth 50 dollars\, that was quite some money\, and those transistors were really not robust\, so I remember Dermot O’ Sullivan telling me the all the IRF I had destroyed during that week will be removed from my salary...” \nAlbert graduates f rom Ecole PolytechniqueFédérale de Lausanne in 1986 and joined directly ESA as Young Graduate Trainee\, YGT. That was the first session of YGTs in ESA. He was hired by ESA and worked 9 years in the power conditioning div ision. Albert left ESA for ETEL as head of space electronic division\, ETE L is a Swiss SME active in the field of motion control . When ETEL decided to leave the space market\, Albert left the company and the space domain\ , and worked in various positions\, as business area manager in machine to ol industry ISMECA\, then as vice director in a \nUniversity of Applied sc ience (HE-ARC)\, to finally close the loop coming back to space and to ESA in the telecom department first as power engineering for Alphasat\, than as system engineering in Neosat and finally project manager for ESAIL and TRITON X. \nAlbert is now enjoying retirement: travelling\, hiking\, skyin g\, hunting and fishing.\n________________________________\n\n\nGeoff Dudl ey\n“Tests in the ESTEC lab on how to recharge Ni-H2 and NiCd cells with frozen electrolyte helped in the Olympus recovery. Another example of su ccessful troubleshooting was an improvement in the management of Cluster-2 Ag-Cd batteries following a faster than expected deterioration in flight performance. They are still operating at a reduced level after 22 years!! !”\nAfter a Post-Doc in solid state electrochemistry at Imperial College London and a period in charge of lithium battery development at the Berec Advanced projects group in Abingdon (UK)\, Geoff Dudley became head of th e Energy Storage Section at ESTEC in November 1982. Retiring in 2011\, he has continued to develop his lithium ion cell model and to follow the in-f light performance of the batteries aboard Mars Express.\n \n DTEND;TZID="W. Europe Standard Time":20231002T182000 DTSTAMP:20230929T062735Z DTSTART;TZID="W. Europe Standard Time":20231002T170000 LAST-MODIFIED:20230927T131539Z LOCATION:Main auditorium PRIORITY:5 SEQUENCE:0 SUMMARY;LANGUAGE=en-gb:Plenary Talk 4: Historic Session TRANSP:OPAQUE UID:040000008200E00074C5B7101A82E008000000009053211B5AA0D901000000000000000 010000000F47D455D9778C34DA408E7E3DE4E4901 X-ALT-DESC;FMTTYPE=text/html:

Historic Session< /span>

Historic evolution of the Power System for Space app lication in Europe

Monday\, 2 Octob er 17:00 -18:20

AUdiTORIUm

Presenters: José A Carrasco (Universidad Miguel Hernández) and Ferdinando Tonicello (ESA)< /span>

This session is a tribute to the individuals who co ntributed their ingenuity to the different power system technologies and s hared their ideas with us through the ESPC. The European space era started with precarious computers and software\, few basic components and not muc h flight heritage and has developed over the years to amazing power system engineering products\, some of which remain in use today. We hope you wil l be inspired by the brilliant minds on stage and by the iconic papers in the booklet\, given with the conference kit\, that paved the way for all o f us and made this conference what it is today.

 \;

Guests:

ALan Weinberg

"\;We were proud of the fact that our designs were copied by the rest of the world and are used even today i n most high power Sats as well as the ISS. Some concepts\, like current-mo de control are also used in commercial industry.”\;

 \;

Alan Weinberg got his first power electronicsexperi ence at Plessey UK designing solid-state standby emergency generato rs and aircraft Cycloconverters. Moved to BAe Stevenage and worked on the GEOS and Bluestreak rocket.

Recruited to Join ESRO at Estec in 1973 working in the powe r electronics section\, where he supported many projects such as OTS\; ECS \; Meteosat\; Olympus\; Hippa rcos\; Hubble Space Telescope and in addition mentoring Spanish tra inees in the art of space circuit design. \;He left ESA in 1995 and as a consultant he was involved in many projects\, the most significant bein g designing the Power System for two prototype spacecraft i.e. the First European GPS Giove-A and Esail Marine Sat. \;He presently runs a con sultancy company.

Ed Bongers

“\;In-orbit short circuits on ECS and the findi ngs of NASA's Long Duration Exposure Facility (LDEF) taught us that both G EO and LEO environment were even more harsh than expected. In-orbit failur e investigations on ECS yielded more knowledge on design and test requirem ents\, which are still applied today.”\;

 \;

After studying physics and a research period of 6 years at Leiden University\, EB joined Fokker Space in 1983. His first So lar Array task was technical responsibility for the Eur eca solar array PVA and electronics and the development of the ARA Mk2 PVA and Thermal Knife HDRS. In 1991 He became head of solar array engi neering at Fokker Space &\; Systems and project manager of many solar a rray development projects. After being company head of Technology and Inno vation from 2006 till 2014\, his last carrier step has been Senior \;E xpert Solar Arrays within Airbus. In the meantime\, he has been leader of the European diode working group and convenor for the ECSS-E-ST-20-08. His final activity was the design\, development\, and qualification of the re cently launched JUICE Solar Array.

He re tired in 2021.

Albert Crausaz

“\;As an anecdote\, at th at time in ‘\;86\, a IRF150 was worth 50 dollars\, that was quite som e money\, and those transistors were really not r obust\, so I remember Dermot O’\; Sullivan telling me the all the IRF I had destroyed during that week will be removed from my salary...”\ ; \;

Albert graduates from Ecole PolytechniqueFédérale de Lausanne in 1986 and joined directly ESA as Young Graduate Trainee\, YGT. That was the first session of YGTs in ESA. He was hired by ESA and worked 9 years in the power conditioning division. Albert left ES A for ETEL as head of space electronic division\, ETEL is a Swiss SME acti ve in the field of motion control . When ETEL decided to leave the space m arket\, Albert left the company and the space domain\, and worked in vario us positions\, as business area manager in machine tool industry ISMECA\, then as vice director in a

University o f Applied science (HE-ARC)\, to finally close the loop coming back to spac e and to ESA in the telecom department first as power engineering for Alphasat\, than as system e ngineering in Neosat and finally project manager for ESAIL and TRITON X.

Albert is now enjoying retirement: travelling\, hiking\, skying\, hunt ing and fishing.

Geoff Dudley

“\;Tests in the ESTEC lab on how to recharge Ni-H2 and NiCd cells with frozen electrolyte helped in the Olympus recovery. \; Another example of successful trou bleshooting was an improvement in the management of Cluster-2 Ag-Cd batter ies following a faster than expected deterioration in flight performance.& nbsp\; They are still operating at a reduced level after 22 years!!!” \;

After a Post-Doc i n solid state electrochemistry at Imperial College London and a period in charge of lithium battery development at the Berec Advanced projects group in Abingdon (UK)\, Geoff Dudley became head of the Energy Storage Section at ESTEC in November 1982. Retiring in 2011\, he has continued to develop his lithium ion cell model and to follow the in- flight performance of the batteries aboard Mars Express.

 \;

X-MICROSOFT-CDO-BUSYSTATUS:BUSY X-MICROSOFT-CDO-IMPORTANCE:1 X-MICROSOFT-DISALLOW-COUNTER:FALSE X-MS-OLK-AUTOFILLLOCATION:FALSE X-MS-OLK-CONFTYPE:0 BEGIN:VALARM TRIGGER:-PT15M ACTION:DISPLAY DESCRIPTION:Reminder END:VALARM END:VEVENT BEGIN:VEVENT CATEGORIES:Green Category CLASS:PUBLIC CREATED:20230616T121547Z DESCRIPTION:PLENARY 3: Monday\, 2 October 16:10- 16:40\nPhotovoltaics on Ea rth vs. Spaceexploration – David Lackner and Jens Ohlmann\n \nSince many years photovoltaic technology was in space THE source for electricit y to power satellites and payloads. Due to the challenge of climate heatin g on earth\, it is well accepted that a transition from today´s energy su pply by fossil fuel towards renewable energy resources is mandatory. It tu rns out that for this transition solar photovoltaic will be globally the m ajor pillar to successfully fight climate change. Thus\, photovoltaic tech nology R&D becomes even more important as in the past. The presentation wi ll address the status and challenges for photovoltaic technologies applied on earth and in space.\n \n DTEND;TZID="W. Europe Standard Time":20231002T164000 DTSTAMP:20230929T062735Z DTSTART;TZID="W. Europe Standard Time":20231002T161000 LAST-MODIFIED:20230927T131401Z LOCATION:Main auditorium PRIORITY:5 SEQUENCE:0 SUMMARY;LANGUAGE=en-gb:Plenary talk 3: Photovoltaics on Earth vs. Space Exp loration TRANSP:OPAQUE UID:040000008200E00074C5B7101A82E00800000000D0B965A959A0D901000000000000000 010000000605B843C750DCA499C4997F596539EAF X-ALT-DESC;FMTTYPE=text/html:

PLENARY 3: Monday\, 2 October 16:1 0- 16:40< /p>

Photovoltaics on Earth vs. Spaceexpl oration –\; David Lackner and Jens Ohlmann

 \;  \ ;  \; \;< /o:p>

Since many years photovoltaic technology w as in space THE source for electricity to power satellites and payloads. D ue to the challenge of climate heating on earth\, it is well accepted that a transition from today´\;s energy supply by fossil fuel towards ren ewable energy resources is mandatory. It turns out that for this transitio n solar photovoltaic will be globally the major pillar to successfully fig ht climate change. Thus\, photovoltaic technology R&\;D becomes even mo re important as in the past. The presentation will address the status and challenges for photovoltaic technologies applied on earth and in space.

 \;

X-MICROSOFT-CDO-BUSYSTATUS:BUSY X-MICROSOFT-CDO-IMPORTANCE:1 X-MICROSOFT-DISALLOW-COUNTER:FALSE X-MS-OLK-AUTOFILLLOCATION:FALSE X-MS-OLK-CONFTYPE:0 BEGIN:VALARM TRIGGER:-PT15M ACTION:DISPLAY DESCRIPTION:Reminder END:VALARM END:VEVENT BEGIN:VEVENT CATEGORIES:Yellow Category CLASS:PUBLIC CREATED:20230616T121547Z DESCRIPTION: \n DTEND;TZID="W. Europe Standard Time":20231002T170000 DTSTAMP:20230929T062735Z DTSTART;TZID="W. Europe Standard Time":20231002T164000 LAST-MODIFIED:20230927T131102Z LOCATION:Exhibition area PRIORITY:5 SEQUENCE:0 SUMMARY;LANGUAGE=en-gb:Coffee break TRANSP:OPAQUE UID:040000008200E00074C5B7101A82E00800000000A0D0438F59A0D901000000000000000 010000000C6DEE8BFE238A142B641C4E314A7436D X-ALT-DESC;FMTTYPE=text/html:< !--[if gte mso 9]>\n\n\n\n\n\n\nfalse\nfalse\nfalse\n\nEN-GB\nX-NONE\nX-NONE\n\n\n\n\n\n\n\n\n\n\n\n\n\n\n\n\n\n\n\n\n\n\n\n\n

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X-MICROSOFT-CDO-BUSYSTATUS:BUSY X-MICROSOFT-CDO-IMPORTANCE:1 X-MICROSOFT-DISALLOW-COUNTER:FALSE X-MS-OLK-AUTOFILLLOCATION:FALSE X-MS-OLK-CONFTYPE:0 BEGIN:VALARM TRIGGER:-PT15M ACTION:DISPLAY DESCRIPTION:Reminder END:VALARM END:VEVENT BEGIN:VEVENT CATEGORIES:Green Category CLASS:PUBLIC CREATED:20230616T121547Z DESCRIPTION:PlENARY 2: Monday\, 2 October 15:40-16:10\nChallenges of human and robotics space exploration - \nStéphanie Lizy - Destrez\n \n Professor in Space Systems Engineering \nHead of Space Advanced Concept re search group \nMSc. & PhD Aerospace Engineering\, \nISAE-SUPAERO \nPhD Aer ospace Engineering\, \nUniversity of Stuttgart\nThis synopsis envisions th e future of robotic and human space exploration\, with a specific focus on the Moon and Mars roadmap. It highlights the crucial connection between e nergy and autonomy\, emphasizing the role of autonomous power systems in s cientific exploration missions. The synopsis explores the challenges posed by perpetual darkness craters and lava tubes\, and underscores the need f or sustainable power solutions to enable these missions. Furthermore\, it investigates how energy autonomy enhances surface mobility on the Moon\, e nabling more efficient and flexible exploration strategies. By addressing the synergy between energy and autonomy\, this synopsis presents a compreh ensive framework for advancing space exploration while ensuring sustainabl e and self-sufficient power solutions. \nStephanie LIZY-DESTREZ is Profess or in Space Systems Engineering at ISAE-SUPAERO (Institut Supérieur de l ’Aéronautique et de l’Espace)\, a worldwide center of excellence in E ngineering research and education in Toulouse (France). She is the head of the Space Advanced Concept research group. She is a graduate of Stuttgart University (Dr-Eng. In 2015) in Germany and ISAE-SUPAERO (PhD in 2015\, M sc in 1995). \nWith more than 27 years of experience working for space age ncies\, industries and universities in space domain\, she conducts researc h and teaching in human and robotic space exploration (Moon\, Mars and ast eroids) and in astrodynamics. Her researches are oriented along two main a xes: first\, trajectory optimization for interplanetary missions (Moon\, M ars and Asteroid)\, with a particular focus on rendezvous in cis-lunar spa ce and secondly\, Human-Robotic interaction during long-term exploration m issions\, with a focus on the impact of confinement and isolation on crew performances. \nAs an engineer\, she had the opportunity to be on console during the main critical operational phases of the ATV Jules Verne mission in 2008. She is the co-founder of the Spaceflight Institute. She serves a s Associate Editor of the Journal of Spacecraft and Rockets and is a forme r member of the Astrodynamics Committee of the IAF (International Astronau tical Federation). She authored and co-authored more than one hundred jour nal and conference papers.\n \n DTEND;TZID="W. Europe Standard Time":20231002T161000 DTSTAMP:20230929T062735Z DTSTART;TZID="W. Europe Standard Time":20231002T154000 LAST-MODIFIED:20230927T131222Z LOCATION:Main auditorium PRIORITY:5 SEQUENCE:0 SUMMARY;LANGUAGE=en-gb:Plenary talk 2: Challenges related to human and robo tics space exploration. TRANSP:OPAQUE UID:040000008200E00074C5B7101A82E008000000000036374559A0D901000000000000000 0100000007658000094F3964E98E060672AEA97D6 X-ALT-DESC;FMTTYPE=text/html:

PlENARY 2: Monday\, 2 October 15:40-16:10

Challe nges of human and robotics space exploration - \;

Sté\;phanie Lizy - Destrez

 \;  \;  \;  \;  \; \;

Professor in Space Systems Engi neering

Head of Space Advanced Concept research group

MSc. &\; PhD Aerospac e Engineering\,

ISAE-SUPAERO

PhD Aerospace Engineering\,

University of Stuttgart

This synopsis envisions the future of robotic and human space exploration \, with a specific focus on the Moon and Mars roadmap. It highlights the c rucial connection between energy and autonomy\, emphasizing the role of au tonomous power systems in scientific exploration missions. The synopsis ex plores the challenges posed by perpetual darkness craters and lava tubes\, and underscores the need for sustainable power s olutions to enable these missions. Furthermore\, it investigates how energ y autonomy enhances surface mobility on the Moon\, enabling more efficient and flexible exploration strategies. By addressing the synergy between en ergy and autonomy\, this synopsis presents a comprehensive framework for a dvancing space exploration while ensuring sustainable and self-sufficient power solutions. \;

Stephanie LIZY-DESTREZ is Professor in Space Systems Engineering at ISA E-SUPAERO (Institut Sup&eacut e\;rieur de l’\;Aé\;ronautique et de l’\;Espace)\, a worldwide center of excellence in Engineering research and education in Toulouse (France). She is the head of the Space Advanced Concept resea rch group. She is a graduate of Stuttgart University (Dr-Eng. In 2015) in Germany and ISAE-SUPAERO (PhD in 2015\, Msc in 1 995).

With more than 27 years of experi ence working for space agencies\, industries and universities in space domain\, she conducts research and teaching in human and robotic space exploration (Moon\, Mars and asteroids) and in astrodyn amics. Her researches are oriented along two main axes: first\, trajectory optimization for interplanetary missions (Moon\, Mars and Asteroid)\, with a particular focus on rendezvous in cis-lunar s pace and secondly\, Human-Robotic interaction during long-term exploration missions\, with a focus on the impact of confinement and isolation on cre w performances.

As an engineer\, she ha d the opportunity to be on console during the main critical operational ph ases of the ATV Jules Verne mission in 2008. She is the co-founder of the Spaceflight Institute. She serves as Associate Editor of the Journal of Sp acecraft and Rockets and is a former member of the Astrodynamics Committee of the IAF (International Astronautical Federation). She authored and co- authored more than one hundred journal and conference papers.

 \; \;&n bsp\; \; \; \; \; \; \; \; \; \; \ ; \;  \; \; \; \;  \; \; \; \; \; \; \; \; \; \;&nbs p\; \; \; \; \; \; \; \; \; \; \;& nbsp\; \; \; \; \; \; \; \; \; \;  \; \; \; \; \; \; \; \; \;

X-MICROSOFT-CDO-BUSYSTATUS:BUSY X-MICROSOFT-CDO-IMPORTANCE:1 X-MICROSOFT-DISALLOW-COUNTER:FALSE X-MS-OLK-AUTOFILLLOCATION:FALSE X-MS-OLK-CONFTYPE:0 BEGIN:VALARM TRIGGER:-PT15M ACTION:DISPLAY DESCRIPTION:Reminder END:VALARM END:VEVENT BEGIN:VEVENT CATEGORIES:Green Category CLASS:PUBLIC CREATED:20230616T121547Z DESCRIPTION:THE ARTEMIS I MISSION -\nCarlos Garcia-Galan\n \nEuropean Service Module Integration Manager\, \nOrion Program\n B.S. Space Sciences\,\nB. S. Electrical Engineering\,\nFlorida Institute o f Technology\nArtemis I has been the first human rated mission returning t o the moon since the 70s. It has been an incredible journey and a fantasti c display of what international cooperation can achieve. This presentation shows the overall mission timeline\, from spacecraft integration and test ing\, launch and return to the Earth. Unbelievable images of the Moon and our beloved blue planet and awesome video footage from onboard the Orion s pacecraft. It also explains some of the key challenges and achievements of the first Artemis mission. An inspiring view for the missions to come. We are back on the Moon! \nNational Aeronautics and Space Administration\, G lenn Research Center\nCarlos Garcia-Galan is the manager of the Orion prog ram’s European Service Module (ESM) Integration Office at NASA’s Glenn Research Center in Cleveland\, Ohio\, since 2021. He brings more than 24 years of experience in human spaceflight to this role\, in which he is res ponsible for the overall integration of the European Space Agency-develope d ESM\, including design activities\, assembly\, integration\, and test wi th other modules of the Orion spacecraft and the Artemis missions. \nA nat ive of Malaga\, Spain\, Garcia-Galan joined the Orion program in 2010 at N ASA’s Lyndon B. Johnson Space Center in Houston\, serving in various key technical and management roles\, including management of integrated space craft design and performance\, mission analysis\, cross-program integratio n\, and launch and flight operations support. \nPrior to joining Orion\, G arcia-Galan was an International Space Station (ISS) flight controller\, w here he supported multiple Space Shuttle-ISS assembly flights and ISS incr ement operations from Mission Control in Houston and in Korolev\, Russia. He also worked for Honeywell Space Systems as a technical lead developing vehicle health management technologies\, including support to the Lockheed Martin team during the initial development of the Orion spacecraft. \nThr oughout his career\, Garcia-Galan has been recognized for his achievements \, including the recipient of the Honeywell Space Systems Engineer of the Year (Houston)\, NASA Silver Achievement Medal\, Exceptional Achievement M edal\, the Johnson Space Center Director’s Commendation\, Orion Program Manager’s Commendation\, and the Silver Snoopy Award.\n \n DTEND;TZID="W. Europe Standard Time":20231002T154000 DTSTAMP:20230929T062735Z DTSTART;TZID="W. Europe Standard Time":20231002T150000 LAST-MODIFIED:20230927T131210Z LOCATION:Main Auditorium PRIORITY:5 SEQUENCE:0 SUMMARY;LANGUAGE=en-gb:Plenary talk 1: Orion mission. TRANSP:OPAQUE UID:040000008200E00074C5B7101A82E008000000009012240A59A0D901000000000000000 01000000032747E7D4DDBCF41A916ED5F1A6616A3 X-ALT-DESC;FMTTYPE=text/html:

THE ARTEMIS I MISSION -

Carlos Garcia-Galan

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European Service Module Int egration Manager\, \;

Orion Program< /p>

B.S. Space Sciences\,

B. S. \;Electrica l Engineering\,

Florida Institute of Technology

Artemis I has been the first human rat ed mission returning to the moon since the 70s. It has been an incredible journey and a fantastic display of what international cooperation can achi eve. This presentation shows the overall mission timeline\, from spacecraf t integration and testing\, launch and return to the Earth. Unbelievable i mages of the Moon and our beloved blue planet and awesome video footage fr om onboard the Orion spacecraft. It also explains some of the key challeng es and achievements of the first Artemis mission. An inspiring view for th e missions to come. We are back on the Moon!

National Aeronautics and \;Space Administrati on\, \;Glenn Research Center

Carlos Garcia-Galan is the manager of the Orion program ’\;s European Service Module (ESM) Integration Office at NASA’\; s Glenn Research Center in Cleveland\, Ohio\, si nce 2021. He brings more than 24 years of experience in human spaceflight to this role\, in which he is responsible for the overall integration of t he European Space Agency-developed ESM\, including design activities\, ass embly\, integration\, and test with other modules of the Orion spacecraft and the Artemis missions.

A native of M alaga\, Spain\, Garcia-Galan joined the Orion program in 2010 at NASA̵ 7\;s Lyndon B. Johnson Space Center in Houston\, serving in various key technical and management roles\, including managem ent of integrated spacecraft design and performance\, mission analysis\, c ross-program integration\, and launch and flight operations support.

Prior to joining Orion\, Garcia-Galan was an International Space Station (ISS) flight controller\, where he supported multiple Space Shuttle-ISS assembly flights and ISS increment operations f rom Mission Control in Houston and in Korolev\, Russia. He also worked for Honeywell Space Systems as a technical lead developing vehicle health man agement technologies\, including support to the Lockheed Martin team durin g the initial development of the Orion spacecraft.

< p class=MsoNormal style='mso-margin-top-alt:auto\;mso-margin-bottom-alt:au to'>Throughout his career\, Garcia-Galan has been recognized for h is achievements\, including the recipient of the Honeywell Space Systems E ngineer of the Year (Houston)\, NASA Silver Achievement Medal\, Exceptiona l Achievement Medal\, the Johnson Space Center D irector’\;s Commendation\, Orion Program Manager’\;s Commendatio n\, and the Silver Snoopy Award.

< span style='mso-tab-count:1'> \; \; \; \; \; \;&nb sp\; \; \; \; \; \; \; \;  \; \; \; \; \; \; \; \;& nbsp\; \; \; \; \; \;

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< td width=107 valign=top style='width:80.0pt\;background:#D2E6E6\;padding:0 cm 5.4pt 0cm 5.4pt\;height:15.0pt'>

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< tr style='mso-yfti-irow:3\;height:15.0pt'>

In augural Speech

from Conference Chair\, City Cou ncil and UMHE

Vé\;ronique Ferle t-Cavrois

- ESPC 2023 Conference Chair - Europea n Space Agency

 \;< o:p>

 \;

 \;

Pablo Ruz Villanueva< /i>

- Major City of Elche

 \;

 \;

 \;

 \;

 \;

 \;

&nb sp\;

Juan José\ ; Ruiz Martí\;nez

- Chancellor University Miguel Herná\;ndez de Elche

 \;

 \;< /span>

Main

Auditorium

 \;

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X-MICROSOFT-CDO-BUSYSTATUS:BUSY X-MICROSOFT-CDO-IMPORTANCE:1 X-MICROSOFT-DISALLOW-COUNTER:FALSE X-MS-OLK-AUTOFILLLOCATION:FALSE X-MS-OLK-CONFTYPE:0 BEGIN:VALARM TRIGGER:-PT15M ACTION:DISPLAY DESCRIPTION:Reminder END:VALARM END:VEVENT BEGIN:VEVENT CATEGORIES:Power Management 2,Orange Category CLASS:PUBLIC CREATED:20230616T121546Z DESCRIPTION:Ferdinando Tonicello – ESA\nCommon failures reference catalog ue\nAt the latest ESPC 2019 a tutorial was held on Failure propagation in electrical and electronic space systems. The relevant tutorial slides are attached.\nOne of the promises made at that time was to compile a “Failu res Reference Catalogue” based on a cooperative initiative\, accepting b oth internal (ESA) and external inputs.\nThanks to the efforts of several people\, we are glad to present a set of such failure cases\, illustrating the issues and the possible solution or solutions to the identified probl ems.\nThe inputs will be presented by the relevant authors.\nThe presented inputs will be shared with the interested audience persons (a file with a ll the compiled cases will be made available after the conference).\n\n DTEND;TZID="W. Europe Standard Time":20231002T125000 DTSTAMP:20230929T062735Z DTSTART;TZID="W. Europe Standard Time":20231002T111000 LAST-MODIFIED:20230927T133428Z LOCATION:Main Auditorium PRIORITY:5 SEQUENCE:0 SUMMARY;LANGUAGE=en-gb:Common failures reference catalogue TRANSP:OPAQUE UID:040000008200E00074C5B7101A82E008000000000021306C58A0D901000000000000000 01000000022EF38632D284B48B007F1495F07C0D7 X-ALT-DESC;FMTTYPE=text/html:\n\n\n\n\n\n\n\n\n

Ferdinando Tonicello – ESA

\n\n

Common failur es reference catalogue

\n\n

At the latest ESPC 2019 a tutorial was held o n Failure propagation in electrical and electronic space systems. The rele vant tutorial slides are attached.

\n\n

One of the promises made at that time was to compile a “Failures Reference Catalogue” based on a cooperative in itiative\, accepting both internal (ESA) and external inputs.

\n\n

Thanks to the efforts of several people\, we are glad to present a set of such failure c ases\, illustrating the issues and the possible solution or solutions to t he identified problems.

\n\n

The inputs will be presented by the relevant authors .

\n\n

The presented inputs will be shared with the interested audience persons ( a file with all the compiled cases will be made available after the confer ence).

\n\n\n X-MICROSOFT-CDO-BUSYSTATUS:BUSY X-MICROSOFT-CDO-IMPORTANCE:1 X-MICROSOFT-DISALLOW-COUNTER:FALSE X-MS-OLK-AUTOFILLLOCATION:FALSE X-MS-OLK-CONFTYPE:0 BEGIN:VALARM TRIGGER:-PT15M ACTION:DISPLAY DESCRIPTION:Reminder END:VALARM END:VEVENT BEGIN:VEVENT CATEGORIES:Solar Generators CLASS:PUBLIC CREATED:20230616T121546Z DESCRIPTION:Carsten Baur – ESA\nSolar cell degradation in space due to pa rticle irradiation\nModelling of solar cell degradation due to particle ir radiation forms an important part of the power analysis for space missions . Two methods are nowadays applied to carry out this kind of analysis – the so-called “equivalent fluence method” that was first described by scientist from JPL (Jet Propulsion Laboratory) and the “displacement dam age dose” method that was introduced by NRL (Naval Research Laboratory). Both methods will be described. Pros and cons of each method will be disc ussed and the way to get consistent results will be provided. An important part of the tutorial will be dedicated to practical examples. Questions l ike: “How do I analyse a given data set?” and “How do I get a remain ing factor for a given mission by using SPENVIS?” will be addressed.\n3. S1\n \n DTEND;TZID="W. Europe Standard Time":20231002T125000 DTSTAMP:20230929T062735Z DTSTART;TZID="W. Europe Standard Time":20231002T111000 LAST-MODIFIED:20230927T154102Z LOCATION:Conference Room PRIORITY:5 SEQUENCE:0 SUMMARY;LANGUAGE=en-gb:Tutorial Solar: Solar cell degradation in space due to particle irradiation TRANSP:OPAQUE UID:040000008200E00074C5B7101A82E0080000000000326D5058A0D901000000000000000 01000000092458CAE00256140B49A43DA4185ECB1 X-ALT-DESC;FMTTYPE=text/html:

Car sten Baur –\; ESA

Solar cell degradation in space due to particle irradiation

Modelling of solar cell degradation due to partic le irradiation forms an important part of the power analysis for space mis sions. Two methods are nowadays applied to carry out this kind of analysis –\; the so-called “\;equivalent fluence method”\; that was first described by scientist from JPL (Jet Propulsion Laboratory) and the “\;displacement damage dose”\; method that was introduced by NR L (Naval Research Laboratory). Both methods will be described. Pros and co ns of each method will be discussed and the way to get consistent results will be provided. An important part of the tutorial will be dedicated to p ractical examples. Questions like: “\;How do I analyse a given data s et?”\; and “\;How do I get a remaining factor for a given missio n by using SPENVIS?”\; will be addressed.

3. S1

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X-MICROSOFT-CDO-BUSYSTATUS:BUSY X-MICROSOFT-CDO-IMPORTANCE:1 X-MICROSOFT-DISALLOW-COUNTER:FALSE X-MS-OLK-AUTOFILLLOCATION:FALSE X-MS-OLK-CONFTYPE:0 BEGIN:VALARM TRIGGER:-PT15M ACTION:DISPLAY DESCRIPTION:Reminder END:VALARM END:VEVENT BEGIN:VEVENT CATEGORIES:Power Management 2,Power Managemen 1 CLASS:PUBLIC CREATED:20230616T121546Z DESCRIPTION:José A. Cobos (UPM. Differential Power)\nSURFACE power deliver y\, the future of High-Performance Computing\nHigh performance computing r equires high performance dc-dc power converters\, supplying low voltages 0 .5-1.2V with adaptive voltage scaling (AVS)\, high current (<1.000A)\, ver y demanding load steps (> 5.000A/ms) and very high and variable voltage ga in (>48) to regulate an input voltage in the range 40-60V. Low losses (pea k efficiency >97%) and high surface current density (>1A/mm2) complete the se high performance requirements.\nProposed “SURFACE power delivery” i s an extension of the “VERTICAL power delivery” trend that is replacin g “LATERAL power delivery” in large chips (>1.000mm2) to reduce copper losses in the power delivery path and maintain supply voltage integrity i n the chip.\nThree novel concepts are described and validated in this talk : a) “extended duty cycle” (60-95%) in both primary and secondary powe r switches\; b) “segmented winding transformer\, SWT” and c) “edge d ynamics”. These three concepts are implemented in a novel “Direct Powe r Converter\, DPx”\n \n DTEND;TZID="W. Europe Standard Time":20231002T104000 DTSTAMP:20230929T062735Z DTSTART;TZID="W. Europe Standard Time":20231002T090000 LAST-MODIFIED:20230927T154003Z LOCATION:Main Auditorium PRIORITY:5 SEQUENCE:0 SUMMARY;LANGUAGE=en-gb:Tutorial: SURFACE power delivery\, the future of Hig h-Performance Computing TRANSP:OPAQUE UID:040000008200E00074C5B7101A82E00800000000209E6DE757A0D901000000000000000 010000000C92153CFB28C884693E6FD24D46E0988 X-ALT-DESC;FMTTYPE=text/html:

José\; A. Cobos (UPM. Differential Power)< /p>

SURFACE power delivery\, the futur e of High-Performance Computing

High performan ce computing requires high performance dc-dc power converters\, supplying low voltages 0.5-1.2V with adaptive voltage scaling (AVS)\, high current ( <\;1.000A)\, very demanding load steps (>\; 5.000A/ ms) and very high and variable voltage gain (>\;48) to regulate a n input voltage in the range 40-60V. Low losses (peak efficiency >\;97%) and high surface current density (>\;1A/mm2) complete these high perfor mance requirements.

Proposed “\;SURFACE power delive ry”\; is an extension of the “\;VERTICAL power delivery”\; trend that is replacing “\;LATERAL power delivery”\; in large ch ips (>\;1.000mm2) to reduce copper losses in the power delive ry path and maintain supply voltage integrity in the chip.

< p>Three novel concepts are described and validated in this talk: a) “ \;extended duty cycle”\; (60-95%) in both primary and secondar y power switches\; b) “\;segmented winding transformer\, SWT&# 8221\; and c) “\;edge dynamics”\;. These three concepts a re implemented in a novel “\;Direct Power Converter\, DPx”\;

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X-MICROSOFT-CDO-BUSYSTATUS:BUSY X-MICROSOFT-CDO-IMPORTANCE:1 X-MICROSOFT-DISALLOW-COUNTER:FALSE X-MS-OLK-AUTOFILLLOCATION:FALSE X-MS-OLK-CONFTYPE:0 BEGIN:VALARM TRIGGER:-PT15M ACTION:DISPLAY DESCRIPTION:Reminder END:VALARM END:VEVENT BEGIN:VEVENT CATEGORIES:Solar Generators CLASS:PUBLIC CREATED:20230616T121545Z DESCRIPTION:Steve Taylor – ESA\nSolar Cells for Space Applications\nThe t utorial gives a brief explanation about how solar cells work and how they are used to make solar arrays for operation in the space environment.\nChr istophe Fongarland - ESA\nNuclear Power\nFor long duration missions that c annot rely on harnessing the external power of the sun\, electrochemical e nergy storage and chemical fuels are simply too low in energy density to p rovide useful amounts of energy. Nuclear processes\, however\, can have hu ge energy densities\, and for this reason\, nuclear power systems (NPS) ar e the only current alternative to solar arrays for long–term supply of p ower in space.\nThis training provides a broad review of NPS\; their appli cations and advantages\, as well as Safety aspects and the associated regu latory implications are briefly explained. For Radioisotopic Power Systems (RPS) the rationale for radioisotope selection is explained\, including t echnical\, safety and availability aspects. A review of power conversion m ethods explains the principles of each\, as well as considering their impo rtant performance characteristics and heritage. The ESA’s ENDURE technol ogy development activities in the field of RPS are summarised and the indu strial and academic resources that will be exploited in the development ar e identified.\n \n DTEND;TZID="W. Europe Standard Time":20231002T104000 DTSTAMP:20230929T062735Z DTSTART;TZID="W. Europe Standard Time":20231002T090000 LAST-MODIFIED:20230927T154019Z LOCATION:Conference Room PRIORITY:5 SEQUENCE:0 SUMMARY;LANGUAGE=en-gb:Tutorial: Solar Cells for Space Applications and Nuc lear Power TRANSP:OPAQUE UID:040000008200E00074C5B7101A82E00800000000909102E557A0D901000000000000000 010000000C92153CFB28C884693E6FD24D46E0988 X-ALT-DESC;FMTTYPE=text/html:

Steve Taylor –\; ESA

Solar Ce lls for Space Applications

The tutorial gives a brief explanation about how solar cells work and how they are used to ma ke solar arrays for operation in the space environment.

< b>Christophe Fongarland - ESA

Nuclear Power

For long duration missions that cannot rely on harnessing t he external power of the sun\, electrochemical energy storage and chemical fuels are simply too low in energy density to provide useful amounts of e nergy. Nuclear processes\, however\, can have huge energy densities\, and for this reason\, nuclear power systems (NPS) are the only current alterna tive to solar arrays for long–\;term supply of power in space.

This training provides a broad review of NPS\; their applicatio ns and advantages\, as well as Safety aspects and the associated regulator y implications are briefly explained. For Radioisotopic Power Systems (RPS) the rationale for radioisotope selection is ex plained\, including technical\, safety and availability aspects. A review of power conversion methods explains the principles of each\, as well as c onsidering their important performance characteristics and heritage. The E SA’\;s ENDURE technology development activities in the field of RPS a re summarised and the industrial and academic resources that will be explo ited in the development are identified.

< o:p> \;

X-MICROSOFT-CDO-BUSYSTATUS:BUSY X-MICROSOFT-CDO-IMPORTANCE:1 X-MICROSOFT-DISALLOW-COUNTER:FALSE X-MS-OLK-AUTOFILLLOCATION:FALSE X-MS-OLK-CONFTYPE:0 BEGIN:VALARM TRIGGER:-PT15M ACTION:DISPLAY DESCRIPTION:Reminder END:VALARM END:VEVENT BEGIN:VEVENT CATEGORIES:Energy Storage and Nuclear CLASS:PUBLIC CREATED:20230616T121545Z DESCRIPTION:Sara Morales Serrano – ESA\nSpace Debris Mitigation Standard evolution and impact on power design subsystem\nWith the recent fast grow th in the number of satellites being launched and operating in Earth orbit in the last years\, the sustainable use of space is an urgent necessity i n order not to jeopardise the use of the most valuable Earth orbits for th e future. The number of launched space objects yearly into the LEO protect ed region today is more than 10 times fold what it was 10 years ago\, rend ering the existing Space Debris Mitigation (SDM) standards insufficient to avoid the space debris proliferation. There is a widespread call for more stringent SDM requirements worldwide.\nESA aims to lead by example in the protection of space environment by developing and implementing a Zero Deb ris policy by 2030 that guarantees the long-term space sustainability. The first step of this proactive approach is already on the way with the publ ication in 2023 of the new ESA Space Debris Mitigation and respective tech nical standard.\nIn this tutorial ESA will introduce the main changes that will be brought by the 2023 ESA Space Debris Mitigation standard and asse ss the impacts these will have on the design of future power systems for d ifferent satellite classes and orbits. The needs for technology evolution and opportunities for innovative solutions will also be presented and disc ussed as well as the ways the power subsystem industry to contribute to th is common effort.\n \n DTEND;TZID="W. Europe Standard Time":20231002T104000 DTSTAMP:20230929T062735Z DTSTART;TZID="W. Europe Standard Time":20231002T090000 LAST-MODIFIED:20230927T154019Z LOCATION:S1 PRIORITY:5 SEQUENCE:0 SUMMARY;LANGUAGE=en-gb:Space Debris Mitigation Standard evolution and impac t on power design subsystem TRANSP:OPAQUE UID:040000008200E00074C5B7101A82E00800000000B04F75C157A0D901000000000000000 010000000C92153CFB28C884693E6FD24D46E0988 X-ALT-DESC;FMTTYPE=text/html:

Sara Morales Serrano  \;–\; ESA

Space Debris Mitigation Standard evolution and impact on power design subsystem

With the recent fast growth in the number of satellites being launched and operati ng in Earth orbit in the last years\, the sustainable use of space is an u rgent necessity in order not to jeopardise the use of the most valuable Ea rth orbits for the future. The number of launched space objects yearly int o the LEO protected region today is more than 10 times fold what it was 10 years ago\, rendering the existing Space Debris Mitigation (SDM) standard s insufficient to avoid the space debris proliferation. There is a widespr ead call for more stringent SDM requirements worldwide.

E SA aims to lead by example in the protection of space environment by devel oping and implementing a Zero Debris policy by 2030 that guarantees the lo ng-term space sustainability. The first step of this proactive approach is already on the way with the publication in 2023 of the new ESA Space Debr is Mitigation and respective technical standard.

In this tutorial ESA will introduce the main changes that will be brought by the 2 023 ESA Space Debris Mitigation standard and assess the impacts these will have on the design of future power systems for different satellite classe s and orbits. The needs for technology evolution and opportunities for inn ovative solutions will also be presented and discussed as well as the ways the power subsystem industry to contribute to this common effort.

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X-MICROSOFT-CDO-BUSYSTATUS:BUSY X-MICROSOFT-CDO-IMPORTANCE:1 X-MICROSOFT-DISALLOW-COUNTER:FALSE X-MS-OLK-AUTOFILLLOCATION:FALSE X-MS-OLK-CONFTYPE:0 BEGIN:VALARM TRIGGER:-PT15M ACTION:DISPLAY DESCRIPTION:Reminder END:VALARM END:VEVENT BEGIN:VEVENT CATEGORIES:Energy Storage and Nuclear CLASS:PUBLIC CREATED:20230927T125258Z DESCRIPTION:Ugo Lafont – ESA\nDevelopment of new technologies matching Eu ropean regulations on materials.\nEuropean regulation on chemical substanc e like REACH have a continuous impact on the materials used for space appl ication leading to ban or restriction of certain subtance directly affecti ng availability of material. Recently\, Per- and polyfluoroalkyl substance s (PFAS) are considered to be drastically restricted due to their impact o n the environment. A first internal survey made by ESA on PFAS used in ESA project has identified 8000-12000 individual items entries\, mostly fluor opolymers like Teflon\, Tefzel\, FEP\, PFA\, PVDF that are use in many mat erials.\nIn additon to such restriction on matterias imposed by European r egulation\, industries need to take into account their carbon foot print w ith the entire production chain. This need to be done by mean of Life Cycl e Assessment (LCA) in order to promote Eco Design. Such change of paradigm is a requierement that will be impose in all future space project.\nIn th is respect the aim of this tutorial is to expose to the particiapant what can be done at material level to meet these future requirements with minim um impact on the industrial chain.\nThe tutorial will bring the audience t o a common understanding regarding LCA and Ecodesign and provide several e xample of ongoing technology development for space application aiming to m eet this requirement. The example provided will also expose the new materi als and processes that should facilitate CO2 impact but as well lower cost \, faster production but still keeping a high level of reliabity.\nThe foc us will be mainly in the field of non-metallic materials. Advance in compo site using bio based species\, vitrimers matrix enabling recycling\, repar ing and self bonding capabilities as well as self-healing capabilities. Fr om the thermoplastics side\, the functional performance of electrically co nductive high performance thermoplastics (like PEEK) processed by additive manufacturing and its applications will be presented. Last\, 4D printing concept that brings new capabilities and design concept will be mentionned focussing on electrically induced shape changing possibilities and bio-i nspired composite in view of mechanism replacement.\n \n \n \n DTEND;TZID="W. Europe Standard Time":20231002T125000 DTSTAMP:20230929T062735Z DTSTART;TZID="W. Europe Standard Time":20231002T111000 LAST-MODIFIED:20230927T154026Z LOCATION:S1 PRIORITY:5 SEQUENCE:0 SUMMARY;LANGUAGE=en-gb:Tutorial: Development of new technologies matching E uropean regulations on materials. TRANSP:OPAQUE UID:040000008200E00074C5B7101A82E00800000000F06D0C4E52F1D901000000000000000 010000000C14314529D28D3489C3C7CA2F0517508 X-ALT-DESC;FMTTYPE=text/html:
< p>Ugo Lafont –\; ESA

Development of new te chnologies matching European regulations on materials.

< p>European regulation on chemical substance like REACH have a continuous i mpact on the materials used for space application leading to ban or restri ction of certain subtance directly affecting ava ilability of material. Recently\, Per- and polyfluoroalkyl substances (PFA S) are considered to be drastically restricted du e to their impact on the environment. A first internal survey made by ESA on PFAS used in ESA project has identified 8000-12000 individual items ent ries\, mostly fluoropolymers like Teflon\, Tefzel\, FEP\, PFA\, PVDF that are use in many materi als.

In additon to such restric tion on matterias imposed by European regulation \, industries need to take into account their carbon foo t print with the entire production chain. This need to be done by m ean of Life Cycle Assessment (LCA) in order to pr omote Eco Design. Such change of paradigm is a requiere ment that will be impose in all future space project.

In this respect the aim of this tutorial is to expose to the particiapant what can be done at material level to meet t hese future requirements with minimum impact on the industrial chain.

The tutorial will bring the audience to a common understandin g regarding LCA and Ecodesign and provide severa l example of ongoing technology development for s pace application aiming to meet this requirement. The example provided wil l also expose the new materials and processes that should facilitate CO2&n bsp\;impact but as well lower cost\, faster production but still keeping a high level of reliabity.

The focus will be mainly in the field of non-metallic materials. Advance in composite using bio based s pecies\, vitrimers matrix enabling recycling\, < span class=SpellE>reparing and self bonding capabilities as well as self-healing capabilities. From the thermoplast ics side\, the functional performance of electrically conductive high performance thermoplastics (like PEEK) processed by a dditive manufacturing and its applications will be presented. Last\, 4D pr inting concept that brings new capabilities and design concept will be mentionned focussing on electrically induced shape changing possibilities and  \;bio-inspired co mposite in view of mechanism replacement.

 \;

 \;

 \;

< /div> X-MICROSOFT-CDO-BUSYSTATUS:BUSY X-MICROSOFT-CDO-IMPORTANCE:1 X-MICROSOFT-DISALLOW-COUNTER:FALSE X-MS-OLK-AUTOFILLLOCATION:FALSE X-MS-OLK-CONFTYPE:0 BEGIN:VALARM TRIGGER:-PT15M ACTION:DISPLAY DESCRIPTION:Reminder END:VALARM END:VEVENT BEGIN:VEVENT CATEGORIES:Power Managemen 1 CLASS:PUBLIC CREATED:20230927T133553Z DESCRIPTION:System 1 (MO1a)\nNicolas Neugnot (ADS)\nMain auditorium\nQuasi- Regulated bus for deep space missions\nDaniele Renzoni (OHB)\nEuropa Clipp er Power Subsystem Implementation and Lessons Learned\nBrandon Burns (JPL) \nHigh voltage power bus: solar array power conversion and power distribut ion\nAusias Garrigos (Elche University)\nA Power Engineer View on Space Ba sed Solar Power\nHenri Barde (ESA retiree)\n \n DTEND;TZID="W. Europe Standard Time":20231003T104000 DTSTAMP:20230929T062735Z DTSTART;TZID="W. Europe Standard Time":20231003T090000 LAST-MODIFIED:20230927T133641Z LOCATION:Main Auditorium PRIORITY:5 SEQUENCE:0 SUMMARY;LANGUAGE=en-gb:System 1 (MO1a) TRANSP:OPAQUE UID:040000008200E00074C5B7101A82E0080000000000BDDA4C58F1D901000000000000000 010000000BC915C3A31A8A24F83ADB52D308AEBDB X-ALT-DESC;FMTTYPE=text/html:
< td width=320 style='width:240.0pt\;border:none\;border-bottom:solid #A6A6A 6 1.0pt\;background:#D2E6E6\;padding:0cm 5.4pt 0cm 5.4pt\;height:14.1pt'>< p class=MsoNormal align=center style='text-align:center'>Main auditorium

System 1 (MO1a)

Nico las Neugnot (ADS)< /o:p>

Quasi-Regulated bus for deep space missions

Daniele Renzoni ( OHB)

Europa Clipper Power Subsystem Implementation and Lessons Learned

Brandon Burns (JPL)

High voltage power bus: solar array power conversion and power distribution

Ausia s Garrigos (Elche University)

A Power Engineer View on Space Based Solar Power

Henri Barde (ESA ret iree)

& nbsp\;

X-MICROSOFT-CDO-BUSYSTATUS:BUSY X-MICROSOFT-CDO-IMPORTANCE:1 X-MICROSOFT-DISALLOW-COUNTER:FALSE X-MS-OLK-AUTOFILLLOCATION:FALSE X-MS-OLK-CONFTYPE:0 BEGIN:VALARM TRIGGER:-PT15M ACTION:DISPLAY DESCRIPTION:Reminder END:VALARM END:VEVENT BEGIN:VEVENT CATEGORIES:Power Management 2 CLASS:PUBLIC CREATED:20230927T133634Z DESCRIPTION:Components 1 (MO1b)\nSven Landstroem (ESA)\nRoom S1\nTPS7H1111- SP 1.5-A\, Ultra-Low Noise\, High PSRR Radiation Hardened Low Dropout Line ar Regulator\nKyle Rakos (TI)\nImpact of Single Event Effects on Modern CO TS DC-DC Buck Converter ICs\nPhilipp Mand (ESA)\nImpact of Radiation on a GaN FET capable PWM Controller IC Prototype for Space Applications\nVolody myr Burkhay (SpaceIC)\nGR716B: mixed-signal rad-hard microcontroller for s witching power and motor control\nMikael Ekström (Frontgrade Gaisler)\n \ n DTEND;TZID="W. Europe Standard Time":20231003T104000 DTSTAMP:20230929T062735Z DTSTART;TZID="W. Europe Standard Time":20231003T090000 LAST-MODIFIED:20230927T133707Z LOCATION:S1 PRIORITY:5 SEQUENCE:0 SUMMARY;LANGUAGE=en-gb:Components 1 (MO1b) TRANSP:OPAQUE UID:040000008200E00074C5B7101A82E0080000000040D1316558F1D901000000000000000 010000000BCE37FBD62FBB2459D19E7A7528383FA X-ALT-DESC;FMTTYPE=text/html:
< td width=320 style='width:240.0pt\;border:solid #A6A6A6 1.0pt\;border-top: none\;background:white\;padding:0cm 5.4pt 0cm 5.4pt\;height:14.1pt'>

Philipp Mand (ESA)

Components 1 (MO1b)

Sven Landstroem (ESA)

Room S1

TPS7H1111-SP 1.5-A\, Ultra-Low Noise\, High PSRR Radiation Hardened Low Dropout Linear Regulator

Kyle Rakos (TI)

Im pact of Single Event Effects on Modern COTS DC-DC Buck Converter ICs< /o:p>

Impact of Radiation on a GaN FET capable PWM Controller IC Prototype for Space App lications

Volodymyr Burkhay (SpaceIC)

GR716B: mixed-signal rad-hard micr ocontroller for switching power and motor control

Mikael Ekström (Frontgrad e Gaisler)

 \;

X-MICROSOFT-CDO-BUSYSTATUS:BUSY X-MICROSOFT-CDO-IMPORTANCE:1 X-MICROSOFT-DISALLOW-COUNTER:FALSE X-MS-OLK-AUTOFILLLOCATION:FALSE X-MS-OLK-CONFTYPE:0 BEGIN:VALARM TRIGGER:-PT15M ACTION:DISPLAY DESCRIPTION:Reminder END:VALARM END:VEVENT BEGIN:VEVENT CATEGORIES:Power Managemen 1 CLASS:PUBLIC CREATED:20230927T133741Z DESCRIPTION:DCDC 1\n(MO2a)\nGiulio Simonelli (ESA)\nMain auditorium\nOn the design of sequentially switched DCX converters for solar array regulation : S3ZVZCS\nCarlos Orts (University of Elche)\nbPOL48V\, a rad-hard 48V DC/ DC Converter for Space and HEP Applications\nNils van der Blij (CERN)\nLow Voltage\, High Current Power Converter for High Power Integrated Circuit\ nPatrick Dubus (ISD SA Greece)\nMicrochip SA50-28 isolated power module: a new dc to dc platform for RH and RT space power\nAmit Gole (Microchip)\n \n DTEND;TZID="W. Europe Standard Time":20231003T125000 DTSTAMP:20230929T062735Z DTSTART;TZID="W. Europe Standard Time":20231003T111000 LAST-MODIFIED:20230927T133937Z LOCATION:Main auditorium PRIORITY:5 SEQUENCE:0 SUMMARY;LANGUAGE=en-gb:DCDC 1 (MO2a) TRANSP:OPAQUE UID:040000008200E00074C5B7101A82E00800000000F0415C8D58F1D901000000000000000 010000000B6FCF5366D30074199C0C247465E54BF X-ALT-DESC;FMTTYPE=text/html:

DCDC 1
(MO2a)

Giulio Simonelli (ESA)< /p>

Main auditorium

< b>On the design of sequentially switched DCX converters for solar array regulation: S3ZVZCS

C arlos Orts (University of Elche)

bPOL48V\, a rad-hard 48V DC/DC Converter fo r Space and HEP Applications

Ni ls van der Blij (CERN)

Low Voltage\, High Current Power Converter for High Pow er Integrated Circuit

Patrick Dubus (ISD SA Greece)

Microchip SA5 0-28 isolated power module: a new dc to dc platform for RH and RT space po wer

Amit Gole (Microchip)

 \;

X-MICROSOFT-CDO-BUSYSTATUS:BUSY X-MICROSOFT-CDO-IMPORTANCE:1 X-MICROSOFT-DISALLOW-COUNTER:FALSE X-MS-OLK-AUTOFILLLOCATION:FALSE X-MS-OLK-CONFTYPE:0 BEGIN:VALARM TRIGGER:-PT15M ACTION:DISPLAY DESCRIPTION:Reminder END:VALARM END:VEVENT BEGIN:VEVENT CATEGORIES:Power Management 2 CLASS:PUBLIC CREATED:20230927T133849Z DESCRIPTION:EP 1\n(MO2b)\nMatthias Gollor (ESA)\nRoom S1\nAnalysis and Desi gn of a Radio Frequency Generator for Gridded Ion Technology Thruster\nMig uel Astudillo Martínez (UPM)\nEvaluation of the Qucs Software for MSR-ER O Electric Propulsion Power Processing Assembly Modelling and Design Check \nDominique Nicolas (ESA)\nComparative of different Direct Drive architect ures\nPablo Fernandez Miaja (University of Oviedo)\nNew developments\, tec hnologies and status for high power Gridded Ion Thrusters Power Processing Units\nMarcos Nunez (Airbus)\n \n DTEND;TZID="W. Europe Standard Time":20231003T125000 DTSTAMP:20230929T062735Z DTSTART;TZID="W. Europe Standard Time":20231003T111000 LAST-MODIFIED:20230927T133917Z LOCATION:S1 PRIORITY:5 SEQUENCE:0 SUMMARY;LANGUAGE=en-gb:EP 1 (MO2b) TRANSP:OPAQUE UID:040000008200E00074C5B7101A82E008000000006082F1B558F1D901000000000000000 0100000001F14ECA0FA76794181812BA5337639DC X-ALT-DESC;FMTTYPE=text/html:
< table class=MsoNormalTable border=0 cellspacing=0 cellpadding=0 width=320 style='width:240.0pt\;border-collapse:collapse\;mso-yfti-tbllook:1184\;mso -padding-alt:0cm 5.4pt 0cm 5.4pt'>

EP 1
(MO2b)

< td width=320 style='width:240.0pt\;background:#FFCCCC\;padding:0cm 5.4pt 0 cm 5.4pt\;height:26.25pt'>

Matthias Gollo r (ESA)

Room S1

Analysis and Design of a Radio Frequency Generator for Gridded Ion T echnology Thruster

Miguel Astudillo Martínez  (UPM)

Evaluation of the Qucs Software for MSR-ERO Electric Propulsion Power Processing Assembly Mod elling and Design Check

Dominique Nicolas (ESA)

Comparative of di fferent Direct Drive architectures

Pablo Fernandez Miaja (University of Oviedo)

New developments\, technologies and status for high power Gridded Ion Thruster s Power Processing Units

Marcos Nunez (Airbus)

 \;

X-MICROSOFT-CDO-BUSYSTATUS:BUSY X-MICROSOFT-CDO-IMPORTANCE:1 X-MICROSOFT-DISALLOW-COUNTER:FALSE X-MS-OLK-AUTOFILLLOCATION:FALSE X-MS-OLK-CONFTYPE:0 BEGIN:VALARM TRIGGER:-PT15M ACTION:DISPLAY DESCRIPTION:Reminder END:VALARM END:VEVENT BEGIN:VEVENT CATEGORIES:Power Managemen 1 CLASS:PUBLIC CREATED:20230927T134005Z DESCRIPTION:Round Table: Power and SAVOIR reference architecture and interf aces\nF. Tonicello (ESA)\nMain auditorium\n \n DTEND;TZID="W. Europe Standard Time":20231003T160000 DTSTAMP:20230929T062735Z DTSTART;TZID="W. Europe Standard Time":20231003T144500 LAST-MODIFIED:20230927T134111Z LOCATION:Main Auditorium PRIORITY:5 SEQUENCE:0 SUMMARY;LANGUAGE=en-gb:Round Table: Power and SAVOIR reference architecture and interfaces TRANSP:OPAQUE UID:040000008200E00074C5B7101A82E00800000000E05F02E358F1D901000000000000000 010000000DEC01822287849428872939CF7071959 X-ALT-DESC;FMTTYPE=text/html:

Round Table: Power and SAVOI R reference architecture and interfaces

F. Tonicello (ESA)

Main auditorium

 \;

X-MICROSOFT-CDO-BUSYSTATUS:BUSY X-MICROSOFT-CDO-IMPORTANCE:1 X-MICROSOFT-DISALLOW-COUNTER:FALSE X-MS-OLK-AUTOFILLLOCATION:FALSE X-MS-OLK-CONFTYPE:0 BEGIN:VALARM TRIGGER:-PT15M ACTION:DISPLAY DESCRIPTION:Reminder END:VALARM END:VEVENT BEGIN:VEVENT CATEGORIES:Red category,Yellow category CLASS:PUBLIC CREATED:20230927T134213Z DESCRIPTION: \n DTEND;TZID="W. Europe Standard Time":20231003T203000 DTSTAMP:20230929T062735Z DTSTART;TZID="W. Europe Standard Time":20231003T200000 LAST-MODIFIED:20230927T134450Z LOCATION:Plaça de Baix PRIORITY:5 SEQUENCE:0 SUMMARY;LANGUAGE=en-gb:Surprise event TRANSP:OPAQUE UID:040000008200E00074C5B7101A82E008000000008008542F59F1D901000000000000000 01000000096521C474C5CD041AEE5928AB61E62F9 X-ALT-DESC;FMTTYPE=text/html:< !--[if gte mso 9]>\n\n\n\n\n\n\nfalse\nfalse\nfalse\n\nEN-GB\nX-NONE\nX-NONE\n\n\n\n\n\n\n\n\n\n\n\n\n\n\n\n\n\n\n\n\n\n\n\n\n < /head>

< o:p> \;

X-MICROSOFT-CDO-BUSYSTATUS:BUSY X-MICROSOFT-CDO-IMPORTANCE:1 X-MICROSOFT-DISALLOW-COUNTER:FALSE X-MS-OLK-AUTOFILLLOCATION:FALSE X-MS-OLK-CONFTYPE:0 BEGIN:VALARM TRIGGER:-PT15M ACTION:DISPLAY DESCRIPTION:Reminder END:VALARM END:VEVENT BEGIN:VEVENT CATEGORIES:Power Managemen 1 CLASS:PUBLIC CREATED:20230927T134509Z DESCRIPTION:System 2 (MO4b)\nChristian Elisabelaer (CNES)\nMain auditorium\ nStatistical Sizing of a Satellite Power Subsystem\nManon Huguenin (ADS)\n Quantitative Comparison of Power Architecture for LEO missions\nPilar Ming orance (ESA)\nMicrosatellite Power System for Deep Space Exploration\nCris tian Torres Vergara (University of Elche)\nModular EPS for small mobile ro botic space systems\nBenjamin Hülsen (DFKI)\n \n DTEND;TZID="W. Europe Standard Time":20231004T104000 DTSTAMP:20230929T062735Z DTSTART;TZID="W. Europe Standard Time":20231004T090000 LAST-MODIFIED:20230927T134549Z LOCATION:Main Auditorium PRIORITY:5 SEQUENCE:0 SUMMARY;LANGUAGE=en-gb:System 2 (MO4b) TRANSP:OPAQUE UID:040000008200E00074C5B7101A82E00800000000403E2C9859F1D901000000000000000 010000000404F918C2414FF4B8B686CF1B01EDE7A X-ALT-DESC;FMTTYPE=text/html:
< /tr>< tr style='mso-yfti-irow:6\;height:14.1pt'>< /tr>

System 2 (MO4b)

< /td>

Christian El isabelaer (CNES)

Main auditorium

< span style='font-size:10.0pt\;font-family:"Arial"\,sans-serif\;mso-fareast -font-family:"Times New Roman"\;color:black\;mso-font-kerning:0pt\;mso-lig atures:none\;mso-fareast-language:EN-GB'>Statistical Sizing of a Satellite Power Subsystem

Manon Huguenin (ADS)

Quantitative Comparison o f Power Architecture for LEO missions

Pilar Mingorance (ESA)< o:p>

Micr osatellite Power System for Deep Space Exploration

Cristian Torres Vergara (University of Elche)

Modular EPS for small mobile robotic space systems

Benjamin Hülsen (DFKI)

 \;

X-MICROSOFT-CDO-BUSYSTATUS:BUSY X-MICROSOFT-CDO-IMPORTANCE:1 X-MICROSOFT-DISALLOW-COUNTER:FALSE X-MS-OLK-AUTOFILLLOCATION:FALSE X-MS-OLK-CONFTYPE:0 BEGIN:VALARM TRIGGER:-PT15M ACTION:DISPLAY DESCRIPTION:Reminder END:VALARM END:VEVENT BEGIN:VEVENT CATEGORIES:Power Management 2 CLASS:PUBLIC CREATED:20230927T134551Z DESCRIPTION:Components 2 (MO3b)\nSalvo Pappalardo (ST)\nRoom S1\nImpact of Radiation on a Point-of-Load IC Prototype for Space Applications\nVolodymy r Burkhay (SpaceIC)\nAdaptation and control of a latching current limiter based on a SiC N-MOSFET\nAbraham Lopez Antuna (University of Oviedo)\nImpa ct of Radiation on a Voltage Clamp IC Prototype for Space Applications\nVo lodymyr Burkhay (SpaceIC)\nDo not harm\; a novel methodology to protect el ectrical failure propagation\, applying safety barriers and using modern a nd inexpensive power electronics devices.\nPablo Hernandez (ESA)\n \n DTEND;TZID="W. Europe Standard Time":20231004T104000 DTSTAMP:20230929T062735Z DTSTART;TZID="W. Europe Standard Time":20231004T090000 LAST-MODIFIED:20230927T134620Z LOCATION:S1 PRIORITY:5 SEQUENCE:0 SUMMARY;LANGUAGE=en-gb:Components 2 (MO3b) TRANSP:OPAQUE UID:040000008200E00074C5B7101A82E00800000000E087B0B159F1D901000000000000000 010000000B5AEE7C55035EB4DBE42214EF506E078 X-ALT-DESC;FMTTYPE=text/html:
< /tr>

Components 2 (MO3b)< /p>

Salvo Pappa lardo (ST)

Room S1

Impact of Radiation on a Point-of-Load IC Prototype for Sp ace Applications

Volodymyr Burkhay (SpaceIC)

Adaptation and control of a latching cur rent limiter based on a SiC N-MOSFET< /span>

Abraham Lopez Antuna (University of Oviedo)

Impact of Radiation on a Voltage Clamp IC Prototype for Space Applications

V olodymyr Burkhay (SpaceIC)

Do not harm\; a novel methodology to protect electrical failure propagation\, applying safety barriers and using modern and inexpe nsive power electronics devices.

Pablo Hernandez (ESA)

 \;

X-MICROSOFT-CDO-BUSYSTATUS:BUSY X-MICROSOFT-CDO-IMPORTANCE:1 X-MICROSOFT-DISALLOW-COUNTER:FALSE X-MS-OLK-AUTOFILLLOCATION:FALSE X-MS-OLK-CONFTYPE:0 BEGIN:VALARM TRIGGER:-PT15M ACTION:DISPLAY DESCRIPTION:Reminder END:VALARM END:VEVENT BEGIN:VEVENT CATEGORIES:Power Managemen 1 CLASS:PUBLIC CREATED:20230927T134627Z DESCRIPTION:DCDC 2\n(MO4a)\nJ.A. Carrasco (UMHE)\nMain auditorium\nFour-swi tch buck-boost based module block for highly modular power architecture\nM iguel Fernandez Costales (University of Oviedo)\nComparison of 100V-28V Sw itched-Capacitor DC-DC Converters Based on Cascaded Buck\, Boost and 3-Lev el Buck Topologies for Space Application\nRegina Ramos (UPM)\nADS SpE Fr - High Efficiency\, Versatile and Space Tolerant Point Of Load\nLucien Leco cq (ADS)\n \n \n \n DTEND;TZID="W. Europe Standard Time":20231004T125000 DTSTAMP:20230929T062735Z DTSTART;TZID="W. Europe Standard Time":20231004T111000 LAST-MODIFIED:20230927T134712Z LOCATION:Main Auditorium PRIORITY:5 SEQUENCE:0 SUMMARY;LANGUAGE=en-gb:DCDC 2 (MO4a) TRANSP:OPAQUE UID:040000008200E00074C5B7101A82E008000000006024CAC659F1D901000000000000000 010000000AC616D22709E5D45BB5E4E18B7723D31 X-ALT-DESC;FMTTYPE=text/html:
< p class=MsoNormal align=center style='text-align:center'>DCDC 2
(MO4a)

J.A. C arrasco (UMHE)

Main au ditorium

Four-switch buck-boost based module block for highly modular power architecture

Migu el Fernandez Costales (University of Oviedo)

Comparison of 100V-28V Switched -Capacitor DC-DC Converters Based on Cascaded Buck\, Boo st and 3-Level Buck Topologies for Space Application

R egina Ramos (UPM)

ADS SpE Fr - High Efficiency\, Versatile and Space Tolerant Point Of Load

Lucien Lecocq (ADS)

&nbs p\;

 \;

< /td>

 \;

X-MICROSOFT-CDO-BUSYSTATUS:BUSY X-MICROSOFT-CDO-IMPORTANCE:1 X-MICROSOFT-DISALLOW-COUNTER:FALSE X-MS-OLK-AUTOFILLLOCATION:FALSE X-MS-OLK-CONFTYPE:0 BEGIN:VALARM TRIGGER:-PT15M ACTION:DISPLAY DESCRIPTION:Reminder END:VALARM END:VEVENT BEGIN:VEVENT CATEGORIES:Power Management 2 CLASS:PUBLIC CREATED:20230927T134719Z DESCRIPTION:Control 1\n(MO3a)\nJesus Oliver (ESA)\nRoom S1\nDecentralized C ontrol for a Fault-Tolerant\, Fully Scalable Microprocessor Power Supply f or Spacecraft Applications\nGregory Almeida (INP)\nA comparative study on experimental loop gain measurement techniques applied to digitally control led buck-type power converters\nChristophe Delepaut (ESA)\nDigital control lers design using the ESA Control Toolbox in MATLAB Simulink\nAngel de Cas tro (Univ Autonoma Madrid)\nDigital control for a modular system of DC/DC converters for primary distribution system\nPablo Zumel (Universidad Carlo s III de Madrid)\n \n DTEND;TZID="W. Europe Standard Time":20231004T125000 DTSTAMP:20230929T062735Z DTSTART;TZID="W. Europe Standard Time":20231004T111000 LAST-MODIFIED:20230927T134803Z LOCATION:S1 PRIORITY:5 SEQUENCE:0 SUMMARY;LANGUAGE=en-gb:Control 1 (MO3a) TRANSP:OPAQUE UID:040000008200E00074C5B7101A82E00800000000A062F0E559F1D901000000000000000 0100000008502FCED24EEC34EA2AD1F92103C6988 X-ALT-DESC;FMTTYPE=text/html:
< /tr>

Digital c ontrol for a modular system of DC/DC converters for primary distribution s ystem

Control 1
(MO3a)< /b>

Jesus Oliver (ESA)

Room S1

Decentralized Control for a Fault-Tolerant\, Full y Scalable Microprocessor Power Supply for Spacecraft Applications

Gregory Almeida (INP)

A comparative study on experimental loop gain me asurement techniques applied to digitally controlled buck-type power conve rters

Christophe Delepaut (ESA)

< span style='font-size:10.0pt\;font-family:"Arial"\,sans-serif\;mso-fareast -font-family:"Times New Roman"\;color:black\;mso-font-kerning:0pt\;mso-lig atures:none\;mso-fareast-language:EN-GB'>Digital controllers design using the ESA Control Toolbox in MATLAB Simulink

Angel de Castro (Univ Autonoma Madrid)

Pa blo Zumel (Universidad Carlos III de Madrid)

 \;

X-MICROSOFT-CDO-BUSYSTATUS:BUSY X-MICROSOFT-CDO-IMPORTANCE:1 X-MICROSOFT-DISALLOW-COUNTER:FALSE X-MS-OLK-AUTOFILLLOCATION:FALSE X-MS-OLK-CONFTYPE:0 BEGIN:VALARM TRIGGER:-PT15M ACTION:DISPLAY DESCRIPTION:Reminder END:VALARM END:VEVENT BEGIN:VEVENT CATEGORIES:Power Managemen 1 CLASS:PUBLIC CREATED:20230927T135122Z DESCRIPTION:PCDU 1\n(MO6b)\nAlberto Lazzeretti (LDO)\nMain auditorium\nFutu re PCDU and PCU for new space\nMourad Merabtene (TAS)\nIsolated Auxiliary Power Supply Designs Using COTS Components\nNils van der Blij (CNES)\nMicr osatellite Solar Array Regulator Digital Twin Development and Validation\n Pablo Casado Perez (UMHE)\n \n \n \n DTEND;TZID="W. Europe Standard Time":20231004T160000 DTSTAMP:20230929T062735Z DTSTART;TZID="W. Europe Standard Time":20231004T144500 LAST-MODIFIED:20230927T135226Z LOCATION:Main Auditorium PRIORITY:5 SEQUENCE:0 SUMMARY;LANGUAGE=en-gb:PCDU 1 (MO6b) TRANSP:OPAQUE UID:040000008200E00074C5B7101A82E00800000000A02AAB765AF1D901000000000000000 010000000AE80AA35F700A148ADF31D14EEC3124F X-ALT-DESC;FMTTYPE=text/html:

PCDU 1
(MO6b)

Alberto Lazzer etti (LDO)

Main auditorium

Future PCDU and PCU for new space

M ourad Merabtene (TAS)

< /td>

< b>Isolated Auxiliary Power Suppl y Designs Using COTS Components

Nils van der Blij (CNES)

Microsatellite Solar Array Regulator Digital Twin Development and Validation

Pablo Casado Perez (UMHE)

 \;

 \;

 \;

X-MICROSOFT-CDO-BUSYSTATUS:BUSY X-MICROSOFT-CDO-IMPORTANCE:1 X-MICROSOFT-DISALLOW-COUNTER:FALSE X-MS-OLK-AUTOFILLLOCATION:FALSE X-MS-OLK-CONFTYPE:0 BEGIN:VALARM TRIGGER:-PT15M ACTION:DISPLAY DESCRIPTION:Reminder END:VALARM END:VEVENT BEGIN:VEVENT CATEGORIES:Power Management 2 CLASS:PUBLIC CREATED:20230927T135219Z DESCRIPTION:Electric Propulsion 2 \n(MO5b)\nAndreas Franke (ESA)\nRoom S1\n Isolated DC/DC Converter for RF generator of a Power Propulsion Unit: topo logy comparison based on GaN semiconductors\nGuillermo Núñez Rodríguez (UPM)\nSatellite Electrical Power Subsystem for Direct-Drive Electrical Pr opulsion\nBenjamin Spitaels (TAS)\nA Robustness Analysis of PPU Anode Powe r Supply To Hall-effect Thruster Flickering Phenomenon\nDominique Nicolas (ESA)\n \n \n \n DTEND;TZID="W. Europe Standard Time":20231004T160000 DTSTAMP:20230929T062735Z DTSTART;TZID="W. Europe Standard Time":20231004T144500 LAST-MODIFIED:20230927T135339Z LOCATION:S1 PRIORITY:5 SEQUENCE:0 SUMMARY;LANGUAGE=en-gb:Electric Propulsion 2 (MO5b) TRANSP:OPAQUE UID:040000008200E00074C5B7101A82E00800000000A0D57E985AF1D901000000000000000 010000000DCD5BED5C39C1A4C95EFE8AD468C4D1C X-ALT-DESC;FMTTYPE=text/html:
< table class=MsoNormalTable border=0 cellspacing=0 cellpadding=0 width=320 style='width:240.0pt\;border-collapse:collapse\;mso-yfti-tbllook:1184\;mso -padding-alt:0cm 5.4pt 0cm 5.4pt'>

E lectric Propulsion 2
(MO5b)

< span style='font-family:"Arial"\,sans-serif\;mso-fareast-font-family:"Time s New Roman"\;color:black\;mso-color-alt:windowtext\;mso-font-kerning:0pt\ ;mso-ligatures:none\;mso-fareast-language:EN-GB'>Andreas Franke (ESA)

Room S1< o:p>

Isolat ed DC/DC Converter for RF generator of a Power Propulsion Unit: topology c omparison based on GaN semiconductors

Guillermo Núñez Rodríguez (UPM)

Satellite Electrical Power Subsystem f or Direct-Drive Electrical Propulsion

< tr style='mso-yfti-irow:6\;height:15.0pt'>

Benjamin Spitaels (TAS)

A Robustness Analysis of PPU Anode Power Supply < span class=GramE>To Hall-effect Thruster Flickering Phenomenon

Dominique Nicolas (ESA)

 \;

& nbsp\;

 \;

X-MICROSOFT-CDO-BUSYSTATUS:BUSY X-MICROSOFT-CDO-IMPORTANCE:1 X-MICROSOFT-DISALLOW-COUNTER:FALSE X-MS-OLK-AUTOFILLLOCATION:FALSE X-MS-OLK-CONFTYPE:0 BEGIN:VALARM TRIGGER:-PT15M ACTION:DISPLAY DESCRIPTION:Reminder END:VALARM END:VEVENT BEGIN:VEVENT CATEGORIES:Power Managemen 1 CLASS:PUBLIC CREATED:20230927T135303Z DESCRIPTION:DCDC 4\n(MO6a)\nHans Jensen (Terma)\nMain auditorium\nHigh Powe r Density Sequential Switching Shunt Regulator Module\nBerk Ince (UZAI)\nS mart Power Supply for FPGA and SoC\nMarkus Plattner (Engineering Minds Mun ich)\nPower Unit for High Power Radars and Altimeters\nErik Mache (Advance d Space Power Equipment)\n \n DTEND;TZID="W. Europe Standard Time":20231004T180000 DTSTAMP:20230929T062735Z DTSTART;TZID="W. Europe Standard Time":20231004T162000 LAST-MODIFIED:20230927T135333Z LOCATION:Main Auditorium PRIORITY:5 SEQUENCE:0 SUMMARY;LANGUAGE=en-gb:DCDC 4 (MO6a) TRANSP:OPAQUE UID:040000008200E00074C5B7101A82E0080000000000B5CAB25AF1D901000000000000000 01000000065A94B06E5D5B44F892A0F3243675805 X-ALT-DESC;FMTTYPE=text/html:

DCDC 4
(MO6a)

Hans Jensen (Ter ma)

Main auditorium

High Power Density Sequential Switching Shunt Regulator Module

Berk Ince (UZAI)

Smart Power Supply for FPGA and SoC

Ma rkus Plattner (Engineering Minds Munich)

Power Unit for High Power Radars an d Altimeters

Erik Mache (Advanced Space Power Equipment)

 \;

X-MICROSOFT-CDO-BUSYSTATUS:BUSY X-MICROSOFT-CDO-IMPORTANCE:1 X-MICROSOFT-DISALLOW-COUNTER:FALSE X-MS-OLK-AUTOFILLLOCATION:FALSE X-MS-OLK-CONFTYPE:0 BEGIN:VALARM TRIGGER:-PT15M ACTION:DISPLAY DESCRIPTION:Reminder END:VALARM END:VEVENT BEGIN:VEVENT CATEGORIES:Power Management 2 CLASS:PUBLIC CREATED:20230927T135345Z DESCRIPTION:Control 3\n(MO5a)\nChristophe Delepaut (ESA)\nRoom S1\nMPPT Fin ite-State Supervisor for Electrical Power System Management in LEO Satelli tes\nSalvatore Sagnelli (AVIO)\nAn On-line Detection Optimization Method o f SSPC Based on Transient Temperature Analysis\nYonggang Chen (Academy of Space Tec. Beijing)\nImpacts of distributed power consumption on the power system stability for a huge power satellite\nKang Li (Academy of Space Te chnology Beijing)\n \n DTEND;TZID="W. Europe Standard Time":20231004T180000 DTSTAMP:20230929T062735Z DTSTART;TZID="W. Europe Standard Time":20231004T162000 LAST-MODIFIED:20230927T135426Z LOCATION:S1 PRIORITY:5 SEQUENCE:0 SUMMARY;LANGUAGE=en-gb:Control 3 (MO5a) TRANSP:OPAQUE UID:040000008200E00074C5B7101A82E00800000000104AF3CB5AF1D901000000000000000 01000000012455E40B1C39E4089B45F771DB23517 X-ALT-DESC;FMTTYPE=text/html:

 \;

X-MICROSOFT-CDO-BUSYSTATUS:BUSY X-MICROSOFT-CDO-IMPORTANCE:1 X-MICROSOFT-DISALLOW-COUNTER:FALSE X-MS-OLK-AUTOFILLLOCATION:FALSE X-MS-OLK-CONFTYPE:0 BEGIN:VALARM TRIGGER:-PT15M ACTION:DISPLAY DESCRIPTION:Reminder END:VALARM END:VEVENT BEGIN:VEVENT CATEGORIES:Power Managemen 1 CLASS:PUBLIC CREATED:20230927T135509Z DESCRIPTION:DCDC 3\n(MO7a)\nErich Strixner (ADS)\nMain auditorium\nModular converter analysis and design for the standardization of the power bus in satellites\nAbraham Lopez Antuna (University of Oviedo)\nA Comparison of T echnologies for the Implementation of Low Voltage\, High Current Power Con verters for High Power Integrated Circuits\nAlan Mathewson (ISD Aerospace Ltd)\nOn the implementation of a DC-DC Power Supply for Reducing Electroma gnetic Interference from Power Converters and Filters\nJosé Carrasco (UMH E)\nBattery Discharge Regulator based on Weinberg Topology for High Power Communication Satellites\nEmre Cetin (UZAY)\n \n DTEND;TZID="W. Europe Standard Time":20231005T104000 DTSTAMP:20230929T062735Z DTSTART;TZID="W. Europe Standard Time":20231005T090000 LAST-MODIFIED:20230927T135553Z LOCATION:Main Auditorium PRIORITY:5 SEQUENCE:0 SUMMARY;LANGUAGE=en-gb:DCDC 3 (MO7a) TRANSP:OPAQUE UID:040000008200E00074C5B7101A82E0080000000070F933FE5AF1D901000000000000000 010000000722C1EC32773494287DFFC29575DDEFA X-ALT-DESC;FMTTYPE=text/html:

Control 3
(MO5a)

Christophe Delepaut ( ESA)

Room S1

MPPT Finite-State Supervisor for Electrical Power System Management in LE O Satellites

Salvatore Sagnelli (AV IO)

An On-line Detection Optimization Method of SSPC Based on Transient Temper ature Analysis

< p class=MsoNormal align=center style='text-align:center'>Yonggang< i> Chen (Academy of Space Tec. B eijing)

Impacts of distributed power consumption on the power system stabili ty for a huge power satellite

Kang Li ( Academy of Space Technology Beijing)

Battery Di scharge Regulator based on Weinberg Topology for High Power Communication Satellites

DCDC 3
(MO7a)

Erich Strixner (ADS)

Main auditorium

Modular converter analysis and design for the standardization of the power bus in satellites

< /td>

Abraham Lopez Antuna (University of Oviedo)

A Comparison of Technologies for the Implementa tion of Low Voltage\, High Current Power Converters for High Power Integra ted Circuits

Alan Mathewson (ISD Aerospace Ltd)

On the implemen tation of a DC-DC Power Supply for Reducing Electromagnetic Interference f rom Power Converters and Filters

José Carrasco (UMHE)

Emre Cetin (UZAY)

 \;

X-MICROSOFT-CDO-BUSYSTATUS:BUSY X-MICROSOFT-CDO-IMPORTANCE:1 X-MICROSOFT-DISALLOW-COUNTER:FALSE X-MS-OLK-AUTOFILLLOCATION:FALSE X-MS-OLK-CONFTYPE:0 BEGIN:VALARM TRIGGER:-PT15M ACTION:DISPLAY DESCRIPTION:Reminder END:VALARM END:VEVENT BEGIN:VEVENT CATEGORIES:Power Management 2 CLASS:PUBLIC CREATED:20230927T135554Z DESCRIPTION:Distribution 1\n(MO7b)\nSergio Alia (Beyond Gravity)\nRoom S1\n Comparative analyses of distribution by LCLs and fuses for 100V applicatio n\nMourad Merabtene (TAS)\nTowards higher current and voltage LCLs\nDavid Marroqui (UMHE)\nLCL performances based on GaN transitors\nMourad Merabten e (TAS)\n \n \n \n DTEND;TZID="W. Europe Standard Time":20231005T104000 DTSTAMP:20230929T062735Z DTSTART;TZID="W. Europe Standard Time":20231005T090000 LAST-MODIFIED:20230927T135624Z LOCATION:S1 PRIORITY:5 SEQUENCE:0 SUMMARY;LANGUAGE=en-gb:Distribution 1 (MO7b) TRANSP:OPAQUE UID:040000008200E00074C5B7101A82E00800000000E0280B195BF1D901000000000000000 01000000057F3BB1AF5343546A22859DB32C31081 X-ALT-DESC;FMTTYPE=text/html:

Distribution 1
(MO7b)

Sergio Alia (Bey ond Gravity)

Room S1

Comparative analyses of distribution by LCLs and fuses for 100V application

Mourad Merabtene (TAS)

Tow ards higher current and voltage LCLs

David Marroqui (UMHE)

LCL performances based on GaN tra nsitors

< p class=MsoNormal align=center style='text-align:center'>Mourad Merabtene (TA S)

& nbsp\;

 \;

 \;

X-MICROSOFT-CDO-BUSYSTATUS:BUSY X-MICROSOFT-CDO-IMPORTANCE:1 X-MICROSOFT-DISALLOW-COUNTER:FALSE X-MS-OLK-AUTOFILLLOCATION:FALSE X-MS-OLK-CONFTYPE:0 BEGIN:VALARM TRIGGER:-PT15M ACTION:DISPLAY DESCRIPTION:Reminder END:VALARM END:VEVENT BEGIN:VEVENT CATEGORIES:Power Managemen 1 CLASS:PUBLIC CREATED:20230927T135631Z DESCRIPTION:GaN 1\n(MO8a)\nMourad Merabtene (TAS) \nMain auditorium\nHigh e fficiency GaN based Resonant reset Forward Converter with Synchronous rect ification for Space applications\nMiguel Gonzalez (TAS)\nGaN FET-based\, s calable DCDC converter development for space and stratospheric application s\nLászló Bagó (C3S LLC)\nGaN Based Solar Power Regulator\nAndreas Isak sson (ASP)\n \n \n \n DTEND;TZID="W. Europe Standard Time":20231005T125000 DTSTAMP:20230929T062735Z DTSTART;TZID="W. Europe Standard Time":20231005T111000 LAST-MODIFIED:20230927T135701Z LOCATION:Main Auditorium PRIORITY:5 SEQUENCE:0 SUMMARY;LANGUAGE=en-gb:GaN 1 (MO8a) TRANSP:OPAQUE UID:040000008200E00074C5B7101A82E008000000003008AD2E5BF1D901000000000000000 0100000000D565FAFC6031A479D70BDFCD12AC931 X-ALT-DESC;FMTTYPE=text/html:
< td width=320 style='width:240.0pt\;border:none\;border-right:solid #A6A6A6 1.0pt\;mso-border-top-alt:solid #A6A6A6 1.0pt\;background:white\;padding: 0cm 5.4pt 0cm 5.4pt\;height:66.0pt'>

High effi ciency GaN based Resonant reset Forward Converte r with Synchronous rectification for Space applications< /b>

< p class=MsoNormal align=center style='text-align:center'>GaN 1
(MO8a)

Mourad Merabtene (TAS)

Main auditorium

Migue l Gonzalez (TAS)

GaN FET-based\, scalable DCDC converter development f or space and stratospheric applications

László Bagó (C3S L LC)

GaN Based Solar Power Regulator

Andreas Isaksson (ASP )

&n bsp\;

 \;

 \;

< /html> X-MICROSOFT-CDO-BUSYSTATUS:BUSY X-MICROSOFT-CDO-IMPORTANCE:1 X-MICROSOFT-DISALLOW-COUNTER:FALSE X-MS-OLK-AUTOFILLLOCATION:FALSE X-MS-OLK-CONFTYPE:0 BEGIN:VALARM TRIGGER:-PT15M ACTION:DISPLAY DESCRIPTION:Reminder END:VALARM END:VEVENT BEGIN:VEVENT CATEGORIES:Power Management 2 CLASS:PUBLIC CREATED:20230927T135712Z DESCRIPTION:Control 2\n(MO8b)\nEsteban Sanchis (UV)\nRoom S1\nHardware-In-t he-Loop model design using the ESA Control Toolbox in MATLAB Simulink\nAng el de Castro (Univ. Autonoma Madrid)\nAnalog Global MPPT Techniques for Co mplex I-V Curves\nCristian Torres Vergara (UMHE)\nSMPT: a sequential MPPT approach for power bus management in space vehicles\nLuigi Schirone (Sapie nza University of Rome)\nA new generation of MPPT based on GaN for EVO PCD U\nPablo Lopez Cenamor (ADS)\n \n DTEND;TZID="W. Europe Standard Time":20231005T125000 DTSTAMP:20230929T062735Z DTSTART;TZID="W. Europe Standard Time":20231005T111000 LAST-MODIFIED:20230927T135743Z LOCATION:S1 PRIORITY:5 SEQUENCE:0 SUMMARY;LANGUAGE=en-gb:Control 2 (MO8b) TRANSP:OPAQUE UID:040000008200E00074C5B7101A82E0080000000080A885475BF1D901000000000000000 010000000C7C15251B0ABBF44965DE4B2EA9DA86F X-ALT-DESC;FMTTYPE=text/html:

Control 2
(MO8b)< /b>

Esteban Sanchis (UV)

Room S1

Hardware-In-the-Loop model design using the ESA Control Toolbox in MATLAB Simulink

Angel de Castro (Univ. Autonoma Madrid)

< span style='font-size:10.0pt\;font-family:"Arial"\,sans-serif\;mso-fareast -font-family:"Times New Roman"\;color:black\;mso-font-kerning:0pt\;mso-lig atures:none\;mso-fareast-language:EN-GB'>Analog Global MPPT Techniques for Complex I-V Curves

Cristian Torres Vergara (UMHE)

SMPT: a sequen tial MPPT approach for power bus management in space vehicles

Luigi Schirone (Sapienza University of Rome)

A new generation of MPPT based on GaN for EVO PCDU

Pablo Lopez Cenamor (ADS)

< o:p> \;

X-MICROSOFT-CDO-BUSYSTATUS:BUSY X-MICROSOFT-CDO-IMPORTANCE:1 X-MICROSOFT-DISALLOW-COUNTER:FALSE X-MS-OLK-AUTOFILLLOCATION:FALSE X-MS-OLK-CONFTYPE:0 BEGIN:VALARM TRIGGER:-PT15M ACTION:DISPLAY DESCRIPTION:Reminder END:VALARM END:VEVENT BEGIN:VEVENT CATEGORIES:Power Managemen 1 CLASS:PUBLIC CREATED:20230927T135802Z DESCRIPTION:PCDU 2\n(MO9a)\nFerdinando Tonicello (ESA)\nMain auditorium\nIn novative COTS Based PCU Solution for Telecommunications Market\nPablo Lope z Cenamor (ADS)\nHigh-Power Modular Power Conditioning and Distribution Un it for an Integrated Microsatellite Avionics Stack\nQuentin Mannes (DSI)\n MSR ERO: PCDU & PPU Subsystem\nPablo Lopez Cenamor (ADS)\n \n DTEND;TZID="W. Europe Standard Time":20231005T160000 DTSTAMP:20230929T062735Z DTSTART;TZID="W. Europe Standard Time":20231005T144500 LAST-MODIFIED:20230927T135836Z LOCATION:Main Auditorium PRIORITY:5 SEQUENCE:0 SUMMARY;LANGUAGE=en-gb:PCDU 2 (MO9a) TRANSP:OPAQUE UID:040000008200E00074C5B7101A82E00800000000606561655BF1D901000000000000000 0100000008DB38426480FEF439F7D4A8DCEF4F779 X-ALT-DESC;FMTTYPE=text/html:

PCDU 2
(MO9a)

Ferdinando Tonicello (ESA)

Main auditorium

In novative COTS Based PCU Solution for Telecommunications Market< /span>

Pablo Lopez Cenamor (ADS)

High-Power Modular Power Conditioning and Distribution Unit for an Integrated Microsatellite Avion ics Stack

Quentin Mannes (DSI)

MS R ERO: PCDU &\; PPU Subsystem

Pablo Lopez Cenamor (ADS)

 \;

X-MICROSOFT-CDO-BUSYSTATUS:BUSY X-MICROSOFT-CDO-IMPORTANCE:1 X-MICROSOFT-DISALLOW-COUNTER:FALSE X-MS-OLK-AUTOFILLLOCATION:FALSE X-MS-OLK-CONFTYPE:0 BEGIN:VALARM TRIGGER:-PT15M ACTION:DISPLAY DESCRIPTION:Reminder END:VALARM END:VEVENT BEGIN:VEVENT CATEGORIES:Power Management 2 CLASS:PUBLIC CREATED:20230927T135838Z DESCRIPTION:System 3\n(MO9b)\nJon Caudepon (OHB)\nRoom S1\nGeneric High Pow er System for manned missions to the Moon and beyond\nEmilio Lapena (ADS)\ nGenerational Change of EMC Verification in Japanese Spacecraft Power Supp ly Systems\nToru Kasai (JAXA)\nOn the Electrical Power System of the ASTRO BIO CubeSat\nLuigi Schirone (Sapienza University of Rome)\n \n DTEND;TZID="W. Europe Standard Time":20231005T160000 DTSTAMP:20230929T062735Z DTSTART;TZID="W. Europe Standard Time":20231005T144500 LAST-MODIFIED:20230927T135909Z LOCATION:S1 PRIORITY:5 SEQUENCE:0 SUMMARY;LANGUAGE=en-gb:System 3 (MO9b) TRANSP:OPAQUE UID:040000008200E00074C5B7101A82E00800000000E021C97A5BF1D901000000000000000 0100000007B49DF263F7F8D4391A444C406960923 X-ALT-DESC;FMTTYPE=text/html:
< table class=MsoNormalTable border=0 cellspacing=0 cellpadding=0 width=320 style='width:240.0pt\;border-collapse:collapse\;mso-yfti-tbllook:1184\;mso -padding-alt:0cm 5.4pt 0cm 5.4pt'>

System 3
(M O9b)

Jon Caudepon (OHB)

Room S1< span style='font-family:"Arial"\,sans-serif\;mso-fareast-font-family:"Time s New Roman"\;mso-font-kerning:0pt\;mso-ligatures:none\;mso-fareast-langua ge:EN-GB'>

Generic High Power System for manned mission s to the Moon and beyond

Emilio Lapena (ADS)

Generational Change of EMC Verification in Japanese Spacecraft Power Supply Systems

Toru Kasai (JAXA)

On the Electrical Power System of the ASTROBIO CubeSat< o:p>

Luigi Schirone (Sapienza University of Rome)

 \;

X-MICROSOFT-CDO-BUSYSTATUS:BUSY X-MICROSOFT-CDO-IMPORTANCE:1 X-MICROSOFT-DISALLOW-COUNTER:FALSE X-MS-OLK-AUTOFILLLOCATION:FALSE X-MS-OLK-CONFTYPE:0 BEGIN:VALARM TRIGGER:-PT15M ACTION:DISPLAY DESCRIPTION:Reminder END:VALARM END:VEVENT BEGIN:VEVENT CATEGORIES:Power Managemen 1 CLASS:PUBLIC CREATED:20230927T135917Z DESCRIPTION:PCDU 3\n(MO10a)\nElectrical Propulsion 3\n(MO12b)\nPablo Lopez (ADS)\nMain auditorium\nPLATO PCDU Design with Maximum Power Point Trackin g\nHans Jensen (Terma)\nA High Voltage and High Power PCDU for Space\nXue long Hou (Shenzhen Aerospace New Power Technology)\nADS SpE Fr - New Space Modular and Versatile PPU 1 to 20kW\nFlorent Guedon (ADS)\nA Multifunctio nal Power Processing Unit (M-PPU) that drives multiple thrusters of differ ent types.\nErik Mache (ASP)\n \n DTEND;TZID="W. Europe Standard Time":20231005T180000 DTSTAMP:20230929T062735Z DTSTART;TZID="W. Europe Standard Time":20231005T162000 LAST-MODIFIED:20230927T140006Z LOCATION:Main Auditorium PRIORITY:5 SEQUENCE:0 SUMMARY;LANGUAGE=en-gb:PCDU 3 (MO10a) and Electrical Propulsion 3 (MO12b) TRANSP:OPAQUE UID:040000008200E00074C5B7101A82E00800000000D0B49D915BF1D901000000000000000 0100000001ACF8C23ED214043A828E522DAE598DD X-ALT-DESC;FMTTYPE=text/html:
< /tr>

PCDU 3
(MO10a)

Electrical Propulsion 3
(MO12b)

Pablo Lopez (ADS)

Main auditorium< /span>

PLATO PCD U Design with Maximum Power Point Tracking

Hans Jen sen (Terma)

A High Voltage and High Power PCDU for Space< /span>

Xue long Hou (Shenzhen Aerospace New Power Technology)

A DS SpE Fr - New Space Modular and Versatile PPU 1 to 20kW

Florent Guedon (ADS)

A Multifunct ional Power Processing Unit (M-PPU) that drives multiple thrusters of diff erent types.

Erik Mache (ASP)

 \;

X-MICROSOFT-CDO-BUSYSTATUS:BUSY X-MICROSOFT-CDO-IMPORTANCE:1 X-MICROSOFT-DISALLOW-COUNTER:FALSE X-MS-OLK-AUTOFILLLOCATION:FALSE X-MS-OLK-CONFTYPE:0 BEGIN:VALARM TRIGGER:-PT15M ACTION:DISPLAY DESCRIPTION:Reminder END:VALARM END:VEVENT BEGIN:VEVENT CATEGORIES:Power Management 2 CLASS:PUBLIC CREATED:20230927T140015Z DESCRIPTION:Units 1\n(MO10b)\nMihalis Tourloukis (ESA)\nRoom S1\nPower and Synchronization Unit for Cameras in Space Applications\nFelice Forrisi (AS P)\nModular Architecture for a Control Unit for a Martian Robotic Arm\nLuc a Zerilli (Leonardo)\nCentralized Power Supply Unit for Active Antenna RF equipment\nMiguel Perez (Sener)\nFlexible buck-converter design using the new ST Rad-hard Power MOSFET\nGiuseppe Camonita (STMicroelectronics)\n \n DTEND;TZID="W. Europe Standard Time":20231005T180000 DTSTAMP:20230929T062735Z DTSTART;TZID="W. Europe Standard Time":20231005T162000 LAST-MODIFIED:20230927T142138Z LOCATION:S1 PRIORITY:5 SEQUENCE:0 SUMMARY;LANGUAGE=en-gb:Units 1 (MO10b) TRANSP:OPAQUE UID:040000008200E00074C5B7101A82E0080000000060905FB45BF1D901000000000000000 0100000005873E5BFB4422843804A7B81946CE28D X-ALT-DESC;FMTTYPE=text/html:
< table class=MsoNormalTable border=0 cellspacing=0 cellpadding=0 width=320 style='width:240.0pt\;border-collapse:collapse\;mso-yfti-tbllook:1184\;mso -padding-alt:0cm 5.4pt 0cm 5.4pt'>

Units 1
(MO10b)

Mihalis Tourlo ukis (ESA)

Room S1

Power and Synchronization Unit for Cameras in Space Applications

Felice Forrisi (ASP)

Modular Architecture for a Control Unit for a Martian Robotic Arm

Luca Zerilli (L eonardo)

Centralized Power Supply Unit for Active Antenna RF equipment

Miguel Perez (Sener)

Flexible buck-converter design using the new ST R ad-hard Power MOSFET

Giuseppe Camonita (STMicroelectronics)

 \;< /p>

X-MICROSOFT-CDO-BUSYSTATUS:BUSY X-MICROSOFT-CDO-IMPORTANCE:1 X-MICROSOFT-DISALLOW-COUNTER:FALSE X-MS-OLK-AUTOFILLLOCATION:FALSE X-MS-OLK-CONFTYPE:0 BEGIN:VALARM TRIGGER:-PT15M ACTION:DISPLAY DESCRIPTION:Reminder END:VALARM END:VEVENT BEGIN:VEVENT CATEGORIES:Power Management 2 CLASS:PUBLIC CREATED:20230927T140133Z DESCRIPTION:Motor 1\n(MO12b)\nTim Strous (ESA)\nRoom S2\nA Dual Three-Phase DC-Link Inverter Prototype Powering a Redundant Space Robotics Motor Driv e\nTilman Wimmer (DLR)\nIntegrated Power Solution for Electrical Motor Con trol in TVC Actuation Applications\nShane O`Donnell (MicroChip)\n \n DTEND;TZID="W. Europe Standard Time":20231005T180000 DTSTAMP:20230929T062735Z DTSTART;TZID="W. Europe Standard Time":20231005T170500 LAST-MODIFIED:20230927T140210Z LOCATION:S2 PRIORITY:5 SEQUENCE:0 SUMMARY;LANGUAGE=en-gb:Motor 1 (MO12b) TRANSP:OPAQUE UID:040000008200E00074C5B7101A82E00800000000B0910CE35BF1D901000000000000000 010000000DF0E058ED1CF1A40B8412306CC5FE089 X-ALT-DESC;FMTTYPE=text/html:

Tilman Wimmer (DLR)

Motor 1
(MO12b)
Tim Strous (ESA)< /span>

Room S2

A Dual Three-Phase DC-Link Inverter Prototype Powering a Redundant Space Robotics Motor Drive

Integrated Power Solution for Electrical Motor C ontrol in TVC Actuation Applications

Shane O`Donnell (MicroChip)< /o:p>

 \;

X-MICROSOFT-CDO-BUSYSTATUS:BUSY X-MICROSOFT-CDO-IMPORTANCE:1 X-MICROSOFT-DISALLOW-COUNTER:FALSE X-MS-OLK-AUTOFILLLOCATION:FALSE X-MS-OLK-CONFTYPE:0 BEGIN:VALARM TRIGGER:-PT15M ACTION:DISPLAY DESCRIPTION:Reminder END:VALARM END:VEVENT BEGIN:VEVENT CATEGORIES:Yellow category CLASS:PUBLIC CREATED:20230927T141935Z DESCRIPTION: \n DTEND;TZID="W. Europe Standard Time":20231005T193000 DTSTAMP:20230929T062735Z DTSTART;TZID="W. Europe Standard Time":20231005T190000 LAST-MODIFIED:20230927T142014Z LOCATION:From Congress Centre (c/ Eugeni D'Or) to Hotel Meliá Alicante PRIORITY:5 SEQUENCE:0 SUMMARY;LANGUAGE=en-gb:Transport to Gala Dinner TRANSP:OPAQUE UID:040000008200E00074C5B7101A82E00800000000F0B7FB675EF1D901000000000000000 0100000007DFE1268CDA6BD4899E9FBA692F62EDC X-ALT-DESC;FMTTYPE=text/html:< !--[if gte mso 9]>\n\n\n\n\n\n\nfalse\nfalse\nfalse\n\nEN-GB\nX-NONE\nX-NONE\n\n\n\n\n\n\n\n\n\n\n\n\n\n\n\n\n\n\n\n\n\n\n\n\n < /head>

< o:p> \;

X-MICROSOFT-CDO-BUSYSTATUS:BUSY X-MICROSOFT-CDO-IMPORTANCE:1 X-MICROSOFT-DISALLOW-COUNTER:FALSE X-MS-OLK-AUTOFILLLOCATION:FALSE X-MS-OLK-CONFTYPE:0 BEGIN:VALARM TRIGGER:-PT15M ACTION:DISPLAY DESCRIPTION:Reminder END:VALARM END:VEVENT BEGIN:VEVENT CATEGORIES:Power Managemen 1 CLASS:PUBLIC CREATED:20230927T142151Z DESCRIPTION:Battery Electronics\n(MO11a)\nBrieuc De Smet (ESA)\nMain audito rium\nDevelopment of an Active Battery Management System for Spacecraft\nA lberto Nunez (Abengoa)\nThe Impact of Modern Battery Cell Technologies on Spacecraft DNEL functionality\nTim Strous (ESA)\nEnd-of-Life Battery Passi vation Management System for Small Satellite Constellations in LEO and GEO \nDavide Istria (Argotec)\nA new battery cell simulator and main frame for EGSE Equipment\nAdam Kiss (Rovsing)\n \n DTEND;TZID="W. Europe Standard Time":20231006T122500 DTSTAMP:20230929T062735Z DTSTART;TZID="W. Europe Standard Time":20231006T104500 LAST-MODIFIED:20230927T142228Z LOCATION:Main Auditorium PRIORITY:5 SEQUENCE:0 SUMMARY;LANGUAGE=en-gb:Battery Electronics (MO11a) TRANSP:OPAQUE UID:040000008200E00074C5B7101A82E00800000000D0A7D5B85EF1D901000000000000000 010000000BC85BEC665FF1149A6B1E34E8C03034E X-ALT-DESC;FMTTYPE=text/html:
< /tr>
< p class=MsoNormal align=center style='text-align:center'>Battery Electronics
(MO11a)< /b>

Brieuc De Smet (ESA)

Main auditorium

Development of an Active Battery Management System for S pacecraft

Alberto Nunez (Ab engoa)

The I mpact of Modern Battery Cell Technologies on Spacecraft DNEL functionality

Tim Strous (ESA)

End-of-Life Battery Passivation Management Syste m for Small Satellite Constellations in LEO and GEO< /p>

Davide Istria (Argotec)< /i>

A new battery cell sim ulator and main frame for EGSE Equipment

Adam Kiss (Rovsing)

 \;

X-MICROSOFT-CDO-BUSYSTATUS:BUSY X-MICROSOFT-CDO-IMPORTANCE:1 X-MICROSOFT-DISALLOW-COUNTER:FALSE X-MS-OLK-AUTOFILLLOCATION:FALSE X-MS-OLK-CONFTYPE:0 BEGIN:VALARM TRIGGER:-PT15M ACTION:DISPLAY DESCRIPTION:Reminder END:VALARM END:VEVENT BEGIN:VEVENT CATEGORIES:Power Management 2 CLASS:PUBLIC CREATED:20230927T142233Z DESCRIPTION:Simulation 1\n(MO11b)\nBruno Samaniego (ESA)\nRoom S1\nCo-simul ation of Electrical propulsion and power systems in Direct Drive applicati ons\nPablo Fernandez Miaja (University of Oviedo)\nFully transient energy balances on EcosimPro\nJorge Ruiz Torralba (OHB)\nOpen-Source GUI for Fast Prototyping of Magnetic Components based on Planar Conductors\nAlberto De lgado (UPM)\nA complete approach on validating satellite electrical and po wer sub-system using Systema\nCamille Sanchez (ADS)\n \n DTEND;TZID="W. Europe Standard Time":20231006T122500 DTSTAMP:20230929T062735Z DTSTART;TZID="W. Europe Standard Time":20231006T104500 LAST-MODIFIED:20230927T142302Z LOCATION:S1 PRIORITY:5 SEQUENCE:0 SUMMARY;LANGUAGE=en-gb:Simulation 1 (MO11b) TRANSP:OPAQUE UID:040000008200E00074C5B7101A82E00800000000B092F1D15EF1D901000000000000000 010000000D1A674ACD88B48428D86C47771E09496 X-ALT-DESC;FMTTYPE=text/html:
< p class=MsoNormal align=center style='text-align:center'>Simulation 1
(MO11b)< span style='font-family:"Arial"\,sans-serif\;mso-fareast-font-family:"Time s New Roman"\;mso-font-kerning:0pt\;mso-ligatures:none\;mso-fareast-langua ge:EN-GB'>

Bruno Samaniego (ESA)

Room S1

Co-simulation of Electrical propulsion and power syst ems in Direct Drive applications

Pablo Fernandez Miaja (University of Oviedo)

Fully transient energy balanc es on EcosimPro

Jorge Ruiz Torralba (OHB)

Open-Source GUI for Fast Prototyping of Magnetic Components based on Pl anar Conductors

Alberto Delgado (UPM)

A complete approach on vali dating satellite electrical and power sub-system using Systema< /span>

Camille Sanchez (ADS)

 \;

X-MICROSOFT-CDO-BUSYSTATUS:BUSY X-MICROSOFT-CDO-IMPORTANCE:1 X-MICROSOFT-DISALLOW-COUNTER:FALSE X-MS-OLK-AUTOFILLLOCATION:FALSE X-MS-OLK-CONFTYPE:0 BEGIN:VALARM TRIGGER:-PT15M ACTION:DISPLAY DESCRIPTION:Reminder END:VALARM END:VEVENT BEGIN:VEVENT CATEGORIES:Power Management 2 CLASS:PUBLIC CREATED:20230927T142305Z DESCRIPTION:GaN 2\n(MO12a)\nArturo Fernandez (ESA)\nRoom S2\nGaN based PCDU for MSR ERO Mission\nMario Gomez Alonso (ADS)\nSize and Efficiency Improv ements Using GaN FETs\nJeremy Ferrell (VPT\, Inc.)\nADS SpE Fr - Multipurp ose power cell with GaN FETs for PCU\nHugues Colas (ADS)\nCOTS-Based modul ar BLDC power stage using GaN-FETs for robotic space application\nBenjamin Hülsen (DFKI)\n \n DTEND;TZID="W. Europe Standard Time":20231006T122500 DTSTAMP:20230929T062735Z DTSTART;TZID="W. Europe Standard Time":20231006T104500 LAST-MODIFIED:20230927T142338Z LOCATION:S2 PRIORITY:5 SEQUENCE:0 SUMMARY;LANGUAGE=en-gb:GaN 2 (MO12a) TRANSP:OPAQUE UID:040000008200E00074C5B7101A82E008000000008073C4E45EF1D901000000000000000 0100000006918F015F654194799AB5182A08D59C7 X-ALT-DESC;FMTTYPE=text/html:
< tr style='mso-yfti-irow:5\;height:48.75pt'>
< p class=MsoNormal align=center style='text-align:center'>GaN 2
(MO12a)

Arturo Fernandez (ESA)

Room S2

GaN based PCDU for MSR ERO Mission< o:p>

Mario Gomez Alonso (ADS)

Size and Efficiency Improvements Using GaN FETs

Jeremy Ferrell (VPT\, Inc .)

A DS SpE Fr - Multipurpose power cell with GaN FET s for PCU

Hugues Colas (ADS)

COTS-Based modular BLDC power stage using GaN-FETs for robotic space application

Benjamin Hülsen (DFKI)

 \;

X-MICROSOFT-CDO-BUSYSTATUS:BUSY X-MICROSOFT-CDO-IMPORTANCE:1 X-MICROSOFT-DISALLOW-COUNTER:FALSE X-MS-OLK-AUTOFILLLOCATION:FALSE X-MS-OLK-CONFTYPE:0 BEGIN:VALARM TRIGGER:-PT15M ACTION:DISPLAY DESCRIPTION:Reminder END:VALARM END:VEVENT END:VCALENDAR