SP 2020+1, Preliminary Program DAY 1 Page 1
DAY 1 : March 17th, 2021 SPACE DEMOCRATIZATION
PLENARY SESSION
CONFERENCE INTRODUCTION 9h00 Louis LE PORTZ, 3AF Chairman, Giorgio SACCOCCIA, Dominique RIBEREAU, Guillermo ORTEGA, Co-Chairs of the conference
E Plenary Round Table #1 : X H AGENCIES MID AND LONG TERM POLICIES I B I 9h20 Joseph ASHBAHER, ESA, Jean -Yves LE GALL, CNES, Walter PELZER, DLR, Christian HAUGLIE-HANSSEN, Norwegian Space Agency, T Graham TURNOCK, UKSA, Kailasavadivoo SIVAN, ISRO, Hitoshi KUNINAKA, JAXA, Giorgio SACCOCCIA, ASI I O Chair : Chiara MANFLETTI, ESA N
a n 10h50 COFFEE BREAK d
N Plenary Round Table #2 : E T PRIMES AND OPERATORS VS SUPPLIERS FOR SPACE TRANSPORTATION and SPACECRAFT W O 11h10 Tommaso MISURI, SITAEL, Christina JETZSCHMANN, Airbus Defence and Space GmbH, Onno VERBENE, NAMMO, R K V. NARAYANAN, LPSC/ISRO, Hervé GILIBERT, ArianeGroup, Guy PEREZ, OHB, Patrick VAN PUT, Bradford and ECAPS, Eric KRUCH, SES I N Chairs : Dominique RIBEREAU, ArianeGroup, Jamila MANSOURI, ESA G
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KEYNOTE SPEECH #1: Space democratization 14h00 Matteo PECCONERI , AVIO S.p.A., IT PARALLEL SESSIONS Room 1 Room 2 Room 3 Room 4 Room 5 Room 6 Room 7 SESSION 01 - ST SESSION 02 - ST SESSION 03 - SC SESSION 04 - SC SESSION 05 - SC SESSION 06 - SC SESSION 07 - SC Lox/Methane Engine developements Solid Rocket Motors Cubesat Propulsion Systems 1 Electric Propulsion 1 Modeling and Simulation 1 Capabilities and Techniques Chemical Thrusters 1
CHAIR 1 Marc VALES, Dassault Aviation, FR Yann TALAMONI, ArianeGroup, FR Alberto GARBAYO, AVS -UK, UK Michele COLETTI, Thales Alenia Space, UK Victor FERNANDEZ (ESA) Mark FORD (ESA) Lorenzo BISI, OHB, SE
CHAIR 2 Simon HYDE (ESA) Marco LEONARDI (ESA) Davina DI CARA (ESA) Jose GONZALEZ DEL AMO (ESA) Helmut CIEZKI, DLR, DE Simone CIARALLI, OHB, SE Ferran VALENCIA (ESA) 00159 - Prometheus: Precursor of new low-cost 00007 - P120C Solid Rocket Motor - Synthesis of 00102 - Development of impulse bit-based 00080 - Development status of the Advanced Cusp 00291 - Demonstrator of a Continuously Operating 00079 - Electric Propulsion Torsional Thrust 00059 - An Overview of the LEROS 2c MMH/MON rocket Engine Family the development of the common propulsive SRM effective thrust control for fine precision Field Thruster propulsion system Divert- and Attitude Control System with Run Balance with wireless microwave power transfer High Performance, Cost Effective Apogee Engine for Ariane 6 and Vega-C propulsion systems on CubeSats Time of One Minute E Pamela Simontacchi Max Vaupel Kyaw Swar Robert Westcott X Tarquinio Germani Sakari Teerikoski Norman Hopfe 14:40 1 ArianeGroup - FR Airbus - DE AVS - Added Value Solutions UK - UK Nammo - GB H EUROPROPULSION - FR GomSpace Sweden - SE Bayern-Chemie Gmbh - DE I B 00097 - Development status of the liquid oxygen 00414 - Ariane 6 & VEGA-C Programs - The P120C 00314 - Assessment of the impact of a 00402 - The design, manufacture, and testing of a 00306 - Assessment of numerical diffusion effects 00263 - The Design, Fabrication And Test Progress 00458 - Effect of Chamber Pressure and Mixture I and methane M10 rocket engine for the Vega-E SRM Nozzle Qualification and Manufacturing miniaturized electric propulsion system on the low powered magnetically shielded krypton Hall in magnetized plasma plume simulations Summary of the Iridium catalysed electrolysis Ratio variation in chamber temperature of Liquid upper stage Transition Phase cubesat technologies effect thruster. thruster rocket thruster T Alberto Modesti Daniele Kajon Yann Talamoni Fabrizio Stesina Thomas Munro-O'Brien Charles Muir Shiju P. Nair I 15:00 2 Universidad Carlos III de Madrid - UC3M - ES O AVIO SpA - IT ArianeGroup - FR Politecnico di Torino - IT University of Southampton - UK Imperial College London - UK Liquid Propulsion Systems Centre - ISRO - IN N
00160 - HYPROB-NEW: recent developments of 00355 - A Sounding Rocket Solid Propellant First 00425 - Miniaturizing a resistojet manufacturing, 00155 - Model of the Space Charge Limited 00559 - A software for computational plasma 00168 - Laser-induced fluorescence technique 00459 - Sensitivity Study on Pulse mode a the LOX/LCH4 research line Stage postproduction analysis and testing Electron Emission from Dispenser Cathodes engineering for European space industry development for Hall thrusters diagnostic in 3D performance in AOCS Thruster due to temperature space variations n Francesco Battista Alexander Weigand Swati Thirumangalath Jan-Philipp Wulfkuehler Dejan Petkow Yordanka Dancheva M Ponnuswamy d 15:20 3 CIRA - IT Bayern-Chemie GmbH - DE VTT & Aurora Propulsion Technologies Oy - FI Technische Universität Dresden - DE SPARC Industries SARL - LU Aerospazio Tecnologie - IT Liquid Propulsion Systems Centre - ISRO - IN N E 00416 - Development of LOX-Methane 00401 - Collecting data on aluminum combustion 00311 - Modular impulsive green monopropellant 00470 - Ariane Group 5A Neutralizer qualification 00111 - Numerical simulation of the plume of a 00115 - A non-invasive HET plasma diagnostic tool 00462 - Devolepment of deep throttling engine for T Technology Demonstrator engine and its oxides in solid rocket motors propulsion system (MIMPS-G) overview Magnetically Enhanced Plasma Thruster based on a 1 MSa/s imaging acquisition platform interplanetry missions featuring narrow-band spectral filtering and quasi W Anish K C Stefania Carlotti Ahmed Nosseir Christian Altmann Simone Di Fede real-time processing Ebin Thomas O 15:40 4 Liquid Propulsion Systems Centre - ISRO - IN Politecnico di Milano - IT TU DELFT x University of Pisa - IT ArianeGroup - DE University of Padova - IT Yordanka Dancheva Indian Space Research Organisation - IN R
Aerospazio Tecnologie - IT K I 00088 - Development of a 25 kN Oxygen-Methane 00526 - Prediction of multi-factor coupling 00117 - Emission characteristics and 1250h 00274 - Developing a 3D Numerical Model of a 00322 - Quartz Crystal Microbalance-based 00495 - Investigation of Low Power Arcjet N Test Chamber ablation of EPDM insulation in two-phase endurance test of a cold electron field emitter Magnetized Vacuum Arc Thruster Examination of Sputtering Phenomena of RF Ion Thruster in Test Facilities at IRS and ESA-ESTEC environment based on CNTs for space applications. Thrusters through Numerical Simulation G Horacio Moreira Adam Obrusnik Le Wang Martin Tajmar Jens Simon Partho Pratim Upadhyay 16:00 5 Omnidea Lda. - PT PlasmaSolve s.r.o. - CZ Northwestern Polytechnical University - CN Technische Universität Dresden - DE DLR - German Aerospace Center - DE Institut für Raumfahrtsysteme - DE
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PARALLEL SESSIONS
Room 1 Room 2 Room 3 Room 4 Room 5 Room 6 Room 7 SESSION 08 - ST SESSION 09 - ST SESSION 10 - SC SESSION 11 - SC SESSION 12 - SC SESSION 13 - SC SESSION 14 - SC Programs Aerospike Nozzles Cubesat Propulsion Systems 2 Electric Propulsion 2 Modeling and Simulation 2 Fluid Systems 1 Chemical Thrusters 2
CHAIR 1 Gérard ORDONNEAU, ONERA, FR Ulf PALMNÄS, SE Alberto GARBAYO, AVS -UK, UK Michele COLETTI, Thales Alenia Space, UK Louis WALPOT (ESA) Markus PEUKERT, OHB, DE Gilles VIGIER ,3AF,FR
CHAIR 2 Johan STEELANT (ESA) Mark FORD (ESA) Kathe DANNEMEYER (ESA) Davina DI CARA (ESA) Bayrem ZITOUNI, OHB, DE Richard SCHWANE (ESA) Chris HUNTER (ESA) 00488 - Technology-driven Selection and Design 00403 - Research Activities in the Development of 00082 - Investigation of Thermal Behaviour of 00150 - Performance characterisation of the 00411 - OpenPlume for EP and CP plume 00020 - Innovative Xenon/Krypton FMS (Feed 00045 - An Overview of the Medium and High for future Korean Launch Systems DemoP1: a LOX/LNG Aerospike Engine Additively Manufactured Green Bi-Propellant Water ElecTrolysis Hall Effect Thruster (WET-HET) modelling: tool developments status Management System) for Electric Propulsion, from Altitude Space Propulsion Test Facilities in Demonstrator Thrusters in CubeSat Applications Using Transient using direct thrust measurements R&D to serial production. Westcott E Daeban Seo Thermal Modelling Bayrem Zitouni Federico Rossi Alexander Schwertheim Pierre Cordesse Matthew Palmer X 16:40 1 KARI - KR Peter Van Den Berg OHB - DE Pangea Aerospace - ES Imperial College London - UK Air Liquide - FR Nammo - GB H Delft University of Technology - NL I B 00587 - Innovations in Propulsion within ESA’S 00406 - Investigation of aerodynamic thrust- 00504 - Study of Plume Impingement on CubeSat 00254 - Design of an experimental ablative pulsed 00424 - Plasma brake deorbiting simulation using 00275 - The Development of Highly Efficient 00339 - Overview of Spacecraft Propulsion Future Launcher Preparatory Programme (FLPP) vector control for aerospike nozzles in cold-gas Structure and Solar Array by Different Propellants plasma thruster for micropropulsion dynamic space environment Miniaturised Proportional Valves Based on Activities in Thales Alenia Space in the UK I Advanced Technology experiments Piezoelectric PZT Actuators T Harshit Saini Scherezade Barquero Pyry Peitso Mark Pollard Kate Underhill Jan Sieder-Katzmann Charles Opoku I 17:00 2 SRM Institute of Science and Technology - IN Universidad Carlos III de Madrid - UC3M - ES Aurora Propulsion Technologies - FI Thales Alenia Space UK - UK ESA - NL Technische Universität Dresden - DE The Open University - UK O N
00330 - VINCI Ignition system qualification and 00480 - ACTiVE – Optimisation of a fluidic thrust 00226 - Experimental Study on Micropropulsion 00247 - Design, Set-Up, and First Ignition of the RF 00582 - Design of a Hollow Cathode Thruster: 00418 - Investigation of hysteresis on propellant 00576 - Fusion energy based space propulsion Flight production and successors vector control on aerospike nozzles Using Dust Explosion of Aluminum/Magnesium Helicon-based Plasma Thruster Concepts, Parameter Study and Initial Test Results flow rate for 10 cm class microwave ion thruster using a compact spherical tokamak a with Water Vapor n Rudi Matthijssen Martin Propst Francesco Romano Norman Gondol Yusuke Yamashita Adam Baker Masaya Murohara 17:20 3 d Aerospace Propulsion Products BV - NL Technische Universität Dresden - DE University of Stuttgart - DE Technische Universität Dresden - DE JAXA - JP Rocket Engineering Ltd - GB The University of Tokyo - JP N E 00222 - Overview of rocket testing at the Westcott 00340 - Design and evaluation of aerospike 00212 - Propulsive Performance Analysis of 00467 - Serial Production of Space Components 00391 - Characterization of a 5kW-class hall 00318 - Ongoing Development of next generation 00049 - Development of a Chemical Thrusters test facility (2018/2019) nozzles for upper stage Energetic Ionic Liquid Mono-Propulsion Systems for Megaconstellations thruster via 2D hybrid simulations Electric Propulsion Fluid Management Systems Plume Contamination Module in the frame of the T for Micro-Spacecrafts Plume Impingement Tool “PITOT” W Edward Moore Francesco Nasuti Nils Hildebrand Jesús Perales-Dĺaz Johan Kuiper Asato Wada Andrea Binci 17:40 4 O Airborne Engineering - GB Sapienza University of Rome - IT AST Advanced Space Technologies GmbH - DE Universidad Carlos III de Madrid - UC3M - ES Bradford Engineering - NL JAXA - JP Thales Alenia Space - IT R K I #N/A 00214 - ENPULSION Nano: A fully integrated 00583 - Electrostatic Pump Development for micro electric propulsion system for Small Satellites Liquid Pulsed Plasma Thrusters N G David Krejci Cristian Dobranszki
18:00 5 Enpulsion - AT University of Southampton - UK
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DAY 2 : March 18th, 2021 NEW BUSINESS, NEW MARKETS PLENARY SESSION Plenary Round Table #3 : European Micro Launchers and Space ports Part 1 : Challenges for European Micro launchers, 9h00 Part 2 : Challenges for European Space ports Chairs : Thilo KRANZ, ESA, Jérôme BRETEAU, ESA, Ulf PALMNÄS, Palmnäs & Co
10h40 COFFEE BREAK PARALLEL SESSIONS Room 1 Room 2 Room 3 Room 4 Room 5 Room 6 Room 7 SESSION 15 - ST SESSION 16 - ST SESSION 17 - SC SESSION 18 - SC SESSION 19 - SC SESSION 20 - SC SESSION 21 - SC Engine control Combustion chamber 1 & Ignition Cubesat Propulsion Systems 3 Electric Propulsion 3 Modeling and Simulation 3 Fluid Systems 2 Chemical Thrusters 3
CHAIR 1 Gérard ORDONNEAU, ONERA, FR Didier BOURY, ArianeGroup, FR Alberto GARBAYO, AVS -UK, UK Olivier DUCHEMIN, SAFRAN SEP Toru SHIMADA, JAXA, JAP Markus PEUKERT, OHB, DE Kate UNDERHILL (ESA)
CHAIR 2 Mark FORD (ESA) Carlos MUNOZ (ESA) Armin HERBERTZ (ESA) Neil WALLACE (ESA) Niccola KUTUFA (ESA) Luca FERRACINA (ESA) Kenichi KIMOTO, IHI, JP 00236 - VEGA-E Upper Stage Engine Control Unit 00043 - Low Order Modeling of High-Frequency 00234 - The concept and development status of 00109 - REGULUS: integration and testing of an 00385 - The study on the performances of the 00208 - European Electronic Pressure Regulator - 00038 - Estimation of thrust performance from with closed-loop control for M10 engine Combustion Instabilities in Liquid Rocket Engines new green propellant propulsion system named iodine electric propulsion system micro cathode arc thruster with different cathode Engineering Model Test Results the experimental results of the combustion of “Pinot-G” materials magnesium wires in water vapor Nicole Segala Alexandre Fougnie Mirko Magarotto Nicholas Solway E Naoki Morita Jinyue Geng Mariko Akiyama 11:00 1 GMV-AD - ES EM2C - FR University of Padova - IT Nammo - GB X IHI Aerospace - JP Beijing Institute of Control Engineering - JP The University of Tokyo - JP H I
00477 - Electrical Regulating Valve for Rocket 00325 - LES simulation for evaluation of acoustic 00057 - Experimental Investigation and In-flight 00085 - New EPIC findings: Impact of Mission 00273 - Simulation-guided engineering of an air- 00465 - Experimental studies on Pressure 00573 - Flow Analysis of a Supersonic Nozzle by B Propulsion Systems response of subcritical coaxial flame submitted to Characterization of Micronewton Ultra-Precision Total Impulse on Technology Selection & breathing thruster concept Regulator for failure mode means of Quantitative Schlieren I high-frequency acoustic fields and Low Noise Proportional Propulsion Prerequisites for Lifetime Qualification via Matthias Günther Technology Analysis Krystof Mrozek J. Nithya Bharathi Emilia-Georgiana Prisacariu T Aurélie Nicole 11:20 2 ArianeGroup - DE Xuhui Liu Birk Wollenhaupt PlasmaSolve s.r.o. - CZ Liquid Propulsion Systems Centre - ISRO - IN Romanian Research and Development Institute for I ONERA - FR Gas Turbines - COMOTI - RO O Beijing Institute of Control Engineering - JP OHB System AG - DE N
00533 - Nonlinear Control of an Expander-Bleed 00078 - Numerical characterization of the acoustic 00287 - Development of a cubesat green 00203 - Electric propulsion alternatives selection 00047 - Use of numerical modelling to assess the 00468 - Flow simulation studies on Pressure 00523 - Delta Qualification of a Normally Closed Rocket Engine using Reinforcement Learning damping in a cold flow experiment with coupled propellant tank with fine CoG control to interplanetary missions influence of the electrostatic configuration on the Regulator for Lunar Lander Module Valve with Shape Memory Alloy Actuator for a cavities electric field in an electrospray thruster Hydrazine applications Kai Dresia Michel Poucet Olga Starinova J. Nithya Bharathi n David Marchal Mobin Yunus Malik Pilar Valles 11:40 3 DLR - German Aerospace Center - DE LIFT ME OFF - UK Samara National Research University - RU Liquid Propulsion Systems Centre - ISRO - IN d CentraleSupelec - FR The University of Manchester - UK ArianeGroup - DE N
00496 - On-Ground and In-Flight evaluation of a 00238 - Investigation of Laser Ignition Systems in 00207 - 0.5N Thruster for Small Satellite 00353 - Mission-driven selection of the propulsion 00585 - Modelling and Optimizing an 00175 - Answering the challenges for Electrical 00536 - Effect of Post Weld Heat Treatment on AA- E Redundant Control Electronics for Variable Thrust LOX/Methane Thrust Chambers Propulsion System Using HAN/HN-Based “Safe” system for INNOSAT platform Electrohydrodynamic Thruster Capacitance Tomography systems in rocket 7075-T6 Pressure Vessel welded by Friction Stir T Liquid Engine in Soft-Landing mission Green Monopropellant HNP225 propulsion tanks Welding for Space Application Sebastian Soller Simone Ciaralli Eduardo Calvo W Kiran Ravikumar Shinji Igarashi Philipp Behruzi Mohamed Khatir 12:00 4 ArianeGroup - DE OHB Sweden AB - SE University of Porto - PT O Liquid Propulsion Systems Centre - ISRO - IN IHI Aerospace - JP ArianeGroup - DE Algerian Space Agency - DZ R K
00095 - 2D Full-Cycle Simulation of Air-Breathing 00395 - Electric Thruster Selection Criteria: a #N/A I Microwave Rocket System Point of View N Kuniyoshi Tabata Christophe Koppel G 12:20 5 The University of Tokyo - JP KopooS Consulting ind. - FR
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KEYNOTE SPEECH #2 : Electric Propulsion Activities at ESA 14:00 Jose GONZALEZ DEL AMO, ESA PARALLEL SESSIONS Room 1 Room 2 Room 3 Room 4 Room 5 Room 6 Room 7 SESSION 22 - ST SESSION 23 - ST SESSION 24 - SC SESSION 25 - SC SESSION 26 - SC SESSION 27 - SC SESSION 28 - SC LRE Turbopumps 1 & electro pumps Combustion chamber 2 Cubesat Propulsion Systems 4 Electric Propulsion 4 New Propulsion Concepts In orbit servicing and debris removal Programs and Projects
CHAIR 1 Victor FERNANDEZ (ESA) Didier BOURY, ArianeGroup, FR Alberto GARBAYO, AVS -UK, UK Olivier DUCHEMIN, SAFRAN SEP Jose GONZALEZ DEL AMO (ESA) Markus PEUKERT, OHB, DE Johan STEELANT (ESA)
CHAIR 2 Marc VALES, Dassault Aviation, FR Simon HYDE (ESA) Louis WALPOT (ESA) Cheryl COLLINGWOOD (ESA) Alain DEMAIRÉ, OHB, SE Jeroen VAN DEN EYNDE (ESA) Simone CIARALLI, OHB, SE 00374 - ArianeGroup R&T activities on Fluid 00081 - Wall Pressure Effects of Nitrogen and 00270 - E X B probe measurements in the plasma 00301 - PN-3 helicon plasma device as a testing 00331 - Preliminary investigations of the 00486 - Active Debris Multi-Removal Mission 00033 - Ariane Group Electric Propulsion 2020 – E Structure Interaction (FSI) for space Hydrogen Coolant Layers in a Transpiration Cooled plume of a 100 W-class Hall thruster facility for plasma propulsion study electromagnetic fields in the far plume of a Based on Electrodynamic Tethers An Overview X turbomachinery Model Scramjet Combustor Helicon Plasma Thruster Thibault Hallouin Dmitry Kutuzov Gabriel Borderes Motta Hans Leiter H Ariane Deneuve Friedolin Strauss Pedro José Jiménez 14:40 1 ICARE - CNRS - FR National research center “Kurchatov institute” - Universidad Carlos III de Madrid - UC3M - ES ArianeGroup - DE I ArianeGroup - FR DLR - German Aerospace Center - DE RU Universidad Carlos III de Madrid - UC3M - ES B I
00549 - Optimization And Performance 00337 - Dependency of Coolant Mass Flow on 00218 - Searching for chaotic behavior in the ion 00143 - Validation of a Xenon Propulsion System 00091 - Plasma acceleration by oscillating electric 00286 - Development of a Thruster Gimbal 00288 - Ongoing Satellite Propulsion Activities at T Characterization At Off-Design Conditions For Heat Flux and Surface Temperature in Rocket current waveforms of a Hall effect thruster Simulation Model with 5-kW class Hall-Effect and magnetic fields Mechanism for Accurate Proximity Operations Bradford Space I Supersonic Impulse Turbine Blades Combustion Chambers Thruster Coupled Tests Agnieszka Szelecka Amnon Fruchtman Marcos Perez William Van Meerbeeck O Robson Hahn Pascal Kringe Michele Coletti 15:00 2 IPPLM - PL H.I.T. - Holon Institute of Technology - IL LIFT ME OFF - UK Bradford Engineering - NL N DLR - German Aerospace Center - DE DLR - German Aerospace Center - DE Thales Alenia Space - IT a
00071 - Experimental Validation of Supersonic 00122 - A comparison between film and 00396 - A numerical parametric investigation on 00471 - Electron and ion properties in the beam 00281 - Faraday cup design for low power electric 00006 - Analysis and verification of in-orbit 00567 - Overview of the space propulsion n Turbines for Launcher applications transpiration cooling performance in a rocket the optimal design and operation of coaxial ECR and discharge of a Helicon plasma source for thrusters fuelling system during development and activities at the CNES Toulouse Space Center combustion chamber thrusters application in spacecraft propulsion breadboard testing d Cosmin Petru Suciu Valentin Hugonnaud Thomas Liénart Stijn Koehler Alvaro Sanchez-Villar Alfio Emanuele Vinci Avichai Elimelech 15:20 3 Romanian Research and Development Institute for Enpulsion - AT CNES - FR N Gas Turbines - COMOTI - RO Delft University of Technology - NL Universidad Carlos III de Madrid - UC3M - ES CNRS - FR Thales Alenia Space UK - UK E T
00578 - Concept for compact electropump for 00182 - Implementation of an Acoustic Modes 00070 - Improvement of a numerical tool for the 00108 - Two-dimensional Full Particle-in-Cell 00145 - An experimental study of the ion injector W thruster engines Calculation Method for an 25 kN Engine with simulation of an Helicon Plasma Thruster Simulation of Magnetic Sails in Formation Flight with C/C-Ipresskon® grids Comparison to the L75 Engine Results O Alexandru-Claudiu Cancescu Nabil Souhair Akane Wada Oleg Peysakhovich R Arthur Durigan Bahdur 15:40 4 Romanian Research and Development Institute for Università di Bologna - IT Tohoku University - JP JSC Kompozit - RU K Gas Turbines - COMOTI - RO CLA - Alcântara Launch Center - BR I N
#N/A 00482 - Subsonic and supersonic combustion in 00110 - Quasi 2D PIC Model of a Magnetically 00023 - Design, Manufacture and Testing of a #N/A 00290 - ESA Propulsion Laboratory at ESTEC G the flight Mach number range from 5 to 6 Enhanced Plasma Thruster Laser Micro-manufactured Electrospray Hole Emitter Luca Bianchi Luciano Galfetti Marco Minute Sahil Maharaj ESA - NL 16:00 5 Politecnico di Milano - IT University of Padova - IT University of Manchester - UK
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PARALLEL SESSIONS Room 1 Room 2 Room 3 Room 4 Room 5 Room 6 Room 7 SESSION 29 - ST SESSION 30 - ST SESSION 31 - SC SESSION 32 - SC SESSION 33 - SC SESSION 34 - SC SESSION 35 - SC LRE Turbopumps 2 Engine/Vehicle Interfaces Cubesat Propulsion Systems 5 Electric Propulsion 5 New propulsion Concepts 2 Hybrid Systems 1 Manufacturing and Processess
CHAIR 1 Lilian PREVOST, (CNES), FR Chris HUNTER (ESA) David KREJCI, Enpulsion, DE Michele COLETTI, Thales Alenia Space, UK Helmut CIEZKI, DLR, DE Davar FEILI (ESA) Sébastien BIANCHI, Air Liquide, FR CHAIR 2 Csaba JEGER (ESA) Gérard ORDONNEAU, ONERA, FR Matthew SMITH (ESA) Jose GONZALEZ DEL AMO (ESA) Mark FORD (ESA) Toru SHIMADA, JAXA, JAP Marco DE ROSA (ESA) 00417 - Mathematical Modeling of Powerhead 00157 - Research on Propellant Slosh Dynamics of 00289 - Endurance Test of PETRUS 5J and 00176 - HEMPT electric propulsion status update 00040 - Modeling the Propellant-less Thrust 00278 - The SpaceDrive Project - Conclusion of 00352 - Development and Qualification of an Test Article for a Semi-Cryogenic Engine a Martian Moon Lander Presentation of a Flight Model Design Obtainable from Quantised Inertia. Mach-Effect-Thruster Experiments on High- Electric Propulsion Thruster Orientation Ernst Bosch Precision Balances in Vacuum Mechanism for Electra GEO satellite E Avinash Chandra Keitaro Anii Christoph Montag Mike Mcculloch Thales - DE Maxime Monette Ashley Hallock 16:40 1 X Liquid Propulsion Systems Centre - ISRO - IN The University of Tokyo - JP University of Stuttgart - DE University of Plymouth - UK Technische Universität Dresden - DE OHB Sweden AB - SE H I B 00537 - Development of High Speed Hybrid 00361 - Drag analysis of a modern lightweight 00272 - Long lifetime solenoid valve for Electric 00192 - Hybrid PIC-Fluid Simulation of a 00104 - Thrust Measurements and Evaluation of 00283 - Hybrid Propulsion System for Deep Space 00224 - Magnetic Field Enhancement of the Quad Bearings for Reusable Pump-Fed Liquid Rocket launch vehicle at high mach numbers Propulsion Systems Waveguide ECR Magnetic Nozzle Plasma Thruster Asymmetric Infrared Laser Resonators for Space CubeSat mission Confinement Thruster (QCT): Design and Early I Engines Propulsion Development of the QCT Phoenix T Ainslie French Bohdan Yurkov Marco Riccardo Inchingolo Fredrik Persson Angelo Pasini Oliver Neunzig Emmanuelle Rosati Azevedo 17:00 2 I CIRA - IT Space Electric Thruster Systems - UA Universidad Carlos III de Madrid - UC3M - ES GomSpace Sweden - SE University of Pisa - IT Technische Universität Dresden - DE AVS - Added Value Solutions UK - UK O N
00569 - Contributions regarding the gas dynamics 00588 - Design optimisation and analysis of very 00112 - MEMS thruster based 6DoF propulsion 00521 - Development activities on the Engineering 00198 - Net-shape Technologies for Low-cost 00541 - Common Propellant Hybrid Propulsion 00493 - Market Entries for SUPREMETM Thrusters: of a turbine with partial admission high power transportation system to Mars system for CubeSats Qualification Model of SITAEL’s 5kW-class Hall Manufacture of Tank Shells and Weld-free COPV System Architecture using Applied-Field Commercialization of Superconductor-based-AF- a thruster unit Liner Magnetoplasmadynamic Thrusters MPD n Alexandru-Claudiu Cancescu Orr Cohen Umut Cindemir Tommaso Andreussi Ralf Becker Marcus Collier-Wright Manuel La Rosa Betancourt 17:20 3 d Romanian Research and Development Institute for ESA - NL GomSpace Sweden - SE Gas Turbines - COMOTI - RO SITAEL - IT TISICS Limited - UK Neutron Star Systems - DE Neutron Star Systems - DE N E 00552 - Versatile water test bench for launchers 00584 - Rocket Engine Digital Twin – Modeling and 00285 - Development of an Innovative Chemical 00044 - Spectral radiance measurements of 00308 - Plasma Acceleration by Electromagnetic 00024 - Comparison of green and conventional 00491 - High Temperature Superconductor based liquid engines turbo-pumps and fluids Simulation Benefits Propulsion Subsystem for 12U Earth Observation SPT140 thrusters Nozzle for an Inertial Electrostatic Confinement rocket propellants: system analysis tool for in- propulsion and power system architectures as T management devices and Telecommunication Missions Cathode: Development and Characterization space propulsion enablers for high power missions W David Jimenez Mena Antoine Iffly Dan Ifrim Marcos Perez Yung-An Chan Lukas Werling Marcus Collier-Wright 17:40 4 O Siemens Digital Industry Software - FR Thales Alenia Space - FR Romanian Research and Development Institute for LIFT ME OFF - UK University of Stuttgart - DE DLR - German Aerospace Center - DE Neutron Star Systems - DE R Gas Turbines - COMOTI - RO K I 00580 - Development of turbines nitrogen feed 00169 - The Evolution of the Liquid Cores in Flash 00012 - Lunar Mission Tanks Using Surface 00013 - Investigation of Next Generation 00268 - High-Accuracy Thrust Measurements of systems for liquid rocket engines turbo-pumps Boiling Liquid Nitrogen Sprays Tension Propellant Management Devices for Combined Propulsion Architectures for Electric the EM Drive and Elimination of False-Positive N test benches Propellant Acquisition and Supply and Chemical Propulsion Effects G Andreas Rees Dan Ifrim Don Jaekle Oscar Jennings Martin Tajmar 18:00 5 DLR - German Aerospace Center - DE Romanian Research and Development Institute for Pmd Technology - US Airbus - GB Technische Universität Dresden - DE Gas Turbines - COMOTI - RO
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DAY 3 : March 19th, 2021 ENVIRONMENT PLENARY SESSION Plenary Round Table #4 : Green propulsion for space applications between the different demands 9h00 of old and new mission conditions, cost reduction, and increasing environmental and health regulations Helmut CIEZKI, DLR
10h40 COFFEE BREAK PARALLEL SESSIONS Room 1 Room 2 Room 3 Room 4 Room 5 Room 6 Room7 SESSION 36 - ST SESSION 37 - ST SESSION 38 - SC SESSION 39 - SC SESSION 40 - SC SESSION 41 - SC SESSION 42 - SC Green & Hybrid Propulsion 1 LUMEN Project Green Propulsion 1 Cold Gas Thrusters Propellants 1 Electric Propulsion 6 ISRU 1
CHAIR 1 Jérôme ANTHOINE, ONERA, FR Stefan SCHLECHTRIEM, DLR, DE Helmut CIEZKI, DLR, DE Gilles VIGIER ,3AF,FR Sébastien BIANCHI, Air Liquide, FR George SCHMIDT, NASA, US Nathalie GIRARD (CNES) E CHAIR 2 David PERIGO (ESA) Marco DE ROSA (ESA) Kenichi KIMOTO, IHI, JP Niccola KUTUFA (ESA) Stephan SCHUSTER (ESA) Kathe DANNEMEYER (ESA) Christophe BONNAL, CNES, FR X 00499 - Preliminary assessments for the 00375 - LUMEN Demonstrator – Project Overview 00312 - A survey on energetic ionic liquid green 00089 - Development of cold gas propulsion 00017 - Using of Iodine as Propellant in Electric 00307 - Performance characteristics and efficiency development of a green storable bipropellant propellants and investigation of feed and system for a Portuguese EO & maritime Thrusters analysis of a microwave cathode - 200 W Hall H rocket engine based on H2O2 Jan Deeken pressurization systems for small satellites high- surveillance satellite thruster system I thrust impulsive propulsion Konstantinos Katsonis Stefania Carlotti DLR - German Aerospace Center - DE Nuno Fernandes Takato Morishita 11:00 1 B Ahmed Nosseir DEDALOS Ltd - GR KEYNOTE SPEECH #3 : Politecnico di Milano - IT Omnidea-RTG GmbH - DE The University of Tokyo - JP I TU DELFT x University of Pisa - IT Lunar ISRU propellant production for T in-situ refueling: Operational I 00363 - Overview of the development of a H2O2 00345 - LUMEN Turbopump – Status of the 00381 - Development of Hydrogen Peroxide based 00257 - Direct Thrust Measurements of an Iodine 00171 - Effects of bias potential inside the water 00297 - Radial particle-in-cell simulations of a Hall challenges and implications for space O based chemical attitude control system for VEGA- Development and Testing Monopropellant Thruster Cold Gas Propulsion System ion thruster on thrust performance Thruster discharge with different anomalous propulsion C transport models N Tobias Traudt Narender Kumar Elena Zorzoli Rossi Yasuho Ataka Bastien Haemmerli Alberto Marĺn-Cebrĺan Laurent SIBILLE, NASA, USA 11:20 2 DLR - German Aerospace Center - DE Liquid Propulsion Systems Centre - ISRO - IN ThrustMe - FR University of Tokyo - JP Nammo Raufoss AS - NO Universidad Carlos III de Madrid - UC3M - ES a n d 00373 - Hydrogen Peroxide RCS on a sounding 00292 - LUMEN Thrust Chamber - Injector 00413 - Development of Catalyst for HAN based 00455 - Proba-2 Cool Gas Generator Experiment: 00061 - The investigation of alternative solid 00090 - Design and preliminary study of a 200W 00016 - Spacecraft Propulsion with ISRU near Mars rocket - a milestone towards launch vehicles and Performance and Stability Monopropellant Thruster 10 years in orbit, experiences and lessons learned propellants in Hall Effect Thrusters Cylindrical Hall Thruster and Venus, Based on CO2 Propellant satellite platforms applications. N Justin Hardi Savitry Kumari Berry Sanders Vlad-George Tirila Tatiana Perrotin Chloe Berenguer Tomasz Noga 11:40 3 E DLR - German Aerospace Center - DE Liquid Propulsion Systems Centre - ISRO - IN HDES Service & Engineering BV - NL University of Southampton - UK Universidad Carlos III de Madrid - UC3M - ES DEDALOS Ltd - GR Łukasiewicz Research Network - Institute of T Aviation - PL W O 00485 - Design of a Hovering Sonding Rocket Stage 00048 - LUMEN Thrust Chamber - flame anchoring 00426 - Influence of hot-firing tests on the 00087 - (X)MET: DESIGN AND TEST OF 00054 - Research on Multiphase Flow and 00056 - Development Status of the ST-40 Hall 00018 - Evaluation of Earth Atmosphere Remnants for Measurements in the High Atmosphere for shear coaxial injectors characteristics and activity of a catalyst for the MICROWAVE ELECTROTHERMAL THRUSTERS Catalytic-Combustion Reaction of Microthruster Thruster Used as Propellant in Electric Thruster Technology R hydrogen peroxide decomposition WITH ARGON and XENON with ADN-Based Monopropellant K Karl Wieland Naumann Michael Börner Danill Shcherbak Chloe Berenguer Santiago Casu Thomas Baxter Xuhui Liu 12:00 4 I Bayern-Chemie GmbH - DE DLR - German Aerospace Center - DE Space Electric Thruster Systems - UA DEDALOS Ltd - GR Heraeus Deutschland GmbH & Co. KG - DE AVS - Added Value Solutions UK - UK Beijing Institute of Control Engineering - JP N G
00233 - Controlling Low Frequency Instability in 00068 - LUMEN – Design of the Regenerative 00195 - About Development Feasibility of a High 00364 - Oxygen and propellant production on Hybrid Rocket Combustion Cooling System for an Expander Bleed Cycle Specific Impulse Thruster with Closed Electron Mars by non-equilibrium plasmas Engine using Methane Drift Jina Kim Vasco Guerra Jan Haemisch Alexander Solodukhin 12:20 5 Konkuk University - KR Universidade de Lisboa - PT DLR - German Aerospace Center - DE SSC Keldysh Research Centre - RU
12:40 LUNCH BREAK SP 2020+1, Preliminary Program DAY 3 Page 8
KEYNOTE SPEECH #4: Can Space Propulsion Reusability turn dreams in reality ? Gilles VIGIER, AAAF 14:00 - A space launcher designer point of view - Jean Philippe DUTHEIL, ArianeGroup, FR - From reusability to space plane daily flights" - Marc VALES, Dassault Aviation, FR PARALLEL SESSIONS Room 1 Room 2 Room 3 Room 4 Room 5 Room 6 Room 7 SESSION 43 - ST SESSION 44 - ST SESSION 45 - SC SESSION 46 - SC SESSION 47 - SC SESSION 48 - SC SESSION 49 - SC Green & Hybrid Propulsion 2 Propellant behavior Green Propulsion 2 Mission Analysis and Flight Experience Propellants 2 Electric Propulsion 7 ISRU 2
CHAIR 1 Jérôme ANTHOINE, ONERA, FR Gilles VIGIER ,3AF,FR Wilhelm DINGERTZ, Bradford Ecaps Stephan SCHUSTER (ESA) Sébastien BIANCHI, Air Liquide, FR Niccola KUTUFA (ESA) Nathalie GIRARD (CNES) CHAIR 2 Dirk GREUEL (ESA) Ferran VALENCIA (ESA) Markus PEUKERT, OHB, DE Yann TALAMONI, ArianeGroup, FR Carlos MUNOZ (ESA) Birk WOLLENHAUPT, OHB, DE Christophe BONNAL, CNES, FR E 00524 - Green Propellants for In-Space Propulsion: 00250 - Experimental study on visualization of gas- 00280 - Ignition investigations of a novel 00444 - Overview of an optimised thrust balance 00191 - Performance analysis of alternative 00264 - Experimental characterisation of the novel 00384 - A Detailed Global Model of Hydrogen in Experimental and Modelling Study on the liquid two-phase flow with self-pressurization for hypergolic ionic liquid with hydrogen peroxide in used for accurate measurements during propellants for a helicon plasma thruster Halo plasma thruster for small satellite Support of Neptune Study X Combustion Chemistry of Ethane/Ethene-Nitrous rocket propellants drop tests qualification endurance testing of an electrical applications H Oxide Mixtures thruster Jiewei Zhou Konstantinos Katsonis Kazuki Yasuda Felix Lauck Silvia Masillo 14:40 1 I Sandra Richter Pierre Moutet Universidad Carlos III de Madrid - UC3M - ES DEDALOS Ltd - GR Muroran Institute Of Technology - JP DLR - German Aerospace Center - DE Surrey Space Centre (SSC) - UK B DLR - German Aerospace Center - DE DACTEM Développement - FR I T 00058 - Development of Hybrid-Hybrid Rocket 00190 - Studies on Thermodynamic Vent System 00379 - 100 mN Green Monopropellant Thruster 00397 - EP plasma plume in-Orbit experiments 00002 - New possibilities on creating apogee 00266 - Hall Thruster ST--25 developed by Space 00494 - ISRU produced hydrogen peroxide as Propulsion Technology and Its Prospect in Space for Cryogenic Propellant Storage Tank. Development propulsion systems with electropump propellant Electric Thruster Systems (SETS) multipurpose fuel for spacecraft propulsion, fuel I Exploration (Verification Test for Jet Mixing with Self Jens Laube supply systems cells, and life support systems. O Pressurization) Tomas Hasanof Stanislav Tolok Jong-Shinn Wu OHB System AG - DE Andrey Kukhta Onno Verberne 15:00 2 N Ryoji Imai Plasma Processes LLC - US Space Electric Thruster Systems - UA National Chiao Tung University - TW Yuzhnoye State Design Office - UA Nammo Raufoss AS - NO Muroran Institute Of Technology - JP a n 00029 - Investigation of novel metallized 00579 - Optimizing by numerical simulation the 00441 - Optimization of the catalytic bed in a 00338 - Plasma Jet Pack (PJP) Technology in-flight 00132 - Investigation of Silver Nanoparticles as 00133 - Advances on low-dimensionality fluid 00386 - Mars Ascent Vehicle Propulsion System monopropellants Anti-Vortex Device for swirling flow reduction decomposition chamber for H2O2/liquid results Novel Catalysts for Hypergolic Hydrocarbon modeling of Hall thruster discharges Design By Using CO2 As An In-Situ Oxidizer d during the drainage of a cryogenic liquid in a tank bipropellant thruster Propellants with Hydrogen Peroxide Compound Maxim Kurilov Luc Herrero Enrique Bello-Benítez Alexandru-Claudiu Cancescu Hugo Quintens Sophie Ricker Ozan Kara 15:20 3 N DLR - German Aerospace Center - DE COMAT - FR Universidad Carlos III de Madrid - UC3M - ES Romanian Research and Development Institute for CNES - FR DLR - German Aerospace Center - DE KOC University - TR E Gas Turbines - COMOTI - RO T W 00527 - Effects of compounds in liquefied 00473 - ECAPS HPGP 1N Thruster Development 00448 - MARS-/EUROPA-INPPS Flagship Missions: 00119 - Performance and Behaviour of 00158 - XJET: Design upgrade and preliminary #N/A methane on rocket engine operation and Implementation – State of the Art and High and Low Power Electric Thrusters, Unconventional Molecular Propellants in a characterization for an electrodeless ECR thruster O Heritage Orbits/Payloads and Co-Flying Satellites Cylindrical Hall Thruster Elke Goos Emmanuelle Rosati Azevedo R Wilhelm Dingertz Frank Jansen Rachel Moloney 15:40 4 K DLR - German Aerospace Center - DE AVS - Added Value Solutions UK - UK Bradford Ecaps - SE DLR - German Aerospace Center - DE University of Surrey - UK I N G #N/A 00067 - ICE: A Modular Water Electrolysis 00025 - Development of Iodine Propellant and 00483 - AIRBUS DS Power Processing Units New #N/A Propulsion System Flow Control Units Suitable for Multiple developments for HET & GIT and technologies Propulsion Systems status Alberto Garbayo Javier Martínez Fernando Javier Pintó Marín 16:00 5 AVS - Added Value Solutions UK - UK ThrustMe - FR Airbus DS - ES
16:20 COFFEE BREAK SP 2020+1, Preliminary Program DAY 3 Page 9
PARALLEL SESSIONS
Room 1 Room 2 Room 3 Room 4 Room 5 SESSION 50 - ST SESSION 51 - ST SESSION 52 - SC SESSION 53 - SC SESSION 54 - SC Manufacturing & Process Modeling Thrust chamber Green Propulsion 3 Electric Propulsion 8 Cathodes CHAIR 1 Sébastien BIANCHI, Air Liquide, FR Gérard ORDONNEAU, ONERA, FR Wilhelm DINGERTZ, Bradford Ecaps Olivier DUCHEMIN, SAFRAN SEP Michele COLETTI, Thales Alenia Space, UK E CHAIR 2 Marc VALES, Dassault Aviation, FR Lilian PREVOST, (CNES), FR Lorenzo BISI, OHB, SE Denis ESTUBLIER (ESA) Birk WOLLENHAUPT, OHB, DE X 00099 - Development of an ALM Thrust Chamber 00240 - Investigation of Liquid Cooling Films for 00094 - Experimental testing of small H2/O2 00100 - Development update of the X-EPT 00131 - Investigation of C12A7 electride as a for VEGA-E M10 Rocket Engine storable propellant rocket engines thrusters in atmospheric and vacuum conditions Microwave Gridded Ion Thruster for the IMPULSE thermionic neutralizer H Propulsion Architecture Daniele Liuzzi Sebastian Soller Razvan Nicoara Nils Gerrit Kottke I Sam Reeve 16:40 1 B AVIO SpA - IT ArianeGroup - DE Romanian Research and Development Institute for Airbus - DE Gas Turbines - COMOTI - RO AVS - Added Value Solutions UK - UK I T I 00219 - Additive manufacture of rocket engine 00259 - Machine Learning Methods for Design and 00064 - Electrolysis Based Water Propulsion for 00421 - HIPATIA: a project for the development of 00153 - Endurance Test of a Heaterless Hollow combustion chambers from CuCrZr (C-18150) Operation of Liquid Propellant Rocket Engines Future 1-Ton Class LEO Mission Satellites the Helicon Plasma Thruster and its associated Cathode using the Emitter Material C12A7 O using the DMLS process technologies to intermediate-high TRLs Electride Guenther Waxenegger-Wilfing Nuno Fernandes N Iain Waugh Mercedes Ruiz Christian Drobny 17:00 2 DLR - German Aerospace Center - DE Omnidea-RTG GmbH - DE Airborne Engineering - UK SENER Aeroespacial - ES Technische Universität Dresden - DE a n d 00220 - Additive manufacture of rocket engine 00362 - Development of a film-cooled thrust 00243 - Conceptual design of dual plates 00295 - Power Processing Unit Activities at Thales 00334 - Helical Plume Instabilities in a 25A LaB6 combustion chambers using the ABD®-900AM chamber component in the ESPSS library throttleable injector for monopropellant thruster: Alenia Space in Belgium Hollow Cathode Nickel superalloy a cold flow study Pierluigi Concio Eric Bourguignon Giulia Becatti N Iain Waugh Yehyun Kim 17:20 3 E Sapienza University of Rome - IT Thales Alenia Space in Belgium - BE University of Pisa - IT Airborne Engineering - UK Korea Advanced Institute of Science and T Technology - KR W O 00165 - Selective laser manufactured cooper alloy 00519 - Injector wall heat transfer quantification 00299 - Optical Investigation on the Hypergolic 00005 - Long-Duration Wear Testing of the 00392 - 2 dimensional modelling of heaterless nozzle for sub-scale thrust chambers in supercritical nitrogen injection Reaction Between Green Liquid Ionics and Highly ASTRAEUS Hall Thruster, Phase I: 50 kg Xe Total hollow cathodes R Concentrated Hydrogen Peroxide Throughput Dmitry Suslov Leandro Barbosa Magalhães Stephen Gabriel K Robert Stützer Ryan Conversano 17:40 4 I DLR - German Aerospace Center - DE University of Beira Interior - PT University of Southampton - UK DLR - German Aerospace Center - DE JPL - US N G
KEYNOTE SPEECH #5: Conclusions of the Space Propulsion Conference, 7th Edition 18:00 Alberto GARBAYO, AVS UK, Helmut CIEZKI, DLR
18:30 END OF CONFERENCE