SAFRAN HERAKLES - THE ATMOSPHERIC REENTRY ASSOCIATION
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2 DEAR MADAM, DEAR SIR, DEAR PROFESSIONALS OF THE ATMOSPHERIC REENTRY, For its 4 th edition after the success of the 2006, 2008 and 2011 conferences, your Arcachon rendez-vous is becoming something like a tradition. It is again a pleasure to bring together in the usual friendly way, scientists from the academic community and industry, PhD students, research and development engineers, management delegates from prime contractors and suppliers companies, agencies representatives, end-users representatives, from Australia, Belgium, France, Germany, Italy, Japan, The Netherlands, Spain Switzerland, Ukraine, Russia. Some months after an European Space Agency Council at Ministerial level, the symposium will give the opportunity to exchange on the latest developments and projects dealing with Atmospheric Reentry. I would like to thank the members of the Program Committee who helped building this program, all of them looking forward to meeting you again in a sunny Arcachon! Yours faithfully, Thierry Leveugle President, The Atmospheric Reentry Association Programme Committee Marie-Hélène ARNAL FRENCH SPACE AGENCY CNES Jean-François BELON AVANTAGE AQUITAINE Jean-Marc BOUILLY ASTRIUM SPACE TRANSPORTATION Franco FOSSATI AVIOSPACE Ludger FROEBEL ASTRIUM SPACE TRANSPORTATION Marc LACOSTE SAFRAN HERAKLES - THE ATMOSPHERIC REENTRY ASSOCIATION Thierry LEVEUGLE THE ATMOSPHERIC REENTRY ASSOCIATION José LONGO EUROPEAN SPACE AGENCY Jean MUYLAERT VON KARMAN INSTITUTE Marcello ONOFRI LA SAPIENZA ROME UNIVERSITY Dominique PIROTAIS CEA CESTA - THE ATMOSPHERIC REENTRY ASSOCIATION Marcello SPAGNULO ITALIAN SPACE AGENCY ASI Hendrik WEIHS GERMAN AEROSPACE CENTER DLR
3 Programme May 27 th, h30-09h30 REGISTRATION 4 TH ARA DAYS WELCOME INTRODUCTION 09h30-09h45 09h45-10h15 10h15-10h45 10h45-11h15 11h15-11h45 11h45-12h15 WELCOME ADDRESS Thierry LEVEUGLE, ARA (France) INVITED KEYNOTE The IXV Development Status and Perspectives (including PRIDE). Giorgio TUMINO, European Space Agency (The Netherlands) PLENARY SESSION The SHEFEX Flight Test and Development Program Hendrik WEIHS, German Aerospace Center DLR (Germany) Aerothermodynamic Technologies Required by ESA in the Next Future José LONGO, European Space Agency (The Netherlands) IXV: System Overview and Program Status Roberto ANGELINI, Thales Alenia Space (Italy) 12h15-12h45 The HOMER Test Vehicle: Industrial Approach to Early Technology Validation Nicolas SAUVAGE, Astrium Space Transportation (France) 12h45-14h30 LUNCH 14h30-14h50 14h50-15h10 AERODYNAMICS - AEROTHERMICS - CFD - 1 A Few Aspects of Gas Flow Simulation for Atmospheric Re-entry Nicolas HEROUARD, CEA-CESTA (France) Aerodynamic Analysis of Unmanned Re-Entry Vehicle Concepts from M=0.3 to 25 F. PETROSINO, CIRA (Italy) TPS - 1 Innovative Thermal Protection and Locking Systems for Re-entry Application Roberto VIOTTO, Thales Alenia Space (Italy) Windward and Nose Assemblies CMC Thermal Protection Systems for the IXV Re-entry Demonstrator Development to Qualification : Tests & Analysis Florent GIRARD, Herakles, Safran Group (France)
4 May 27 th, h10-15h30 15h30-15h50 AERODYNAMICS - AEROTHERMICS - CFD - 1 Experimental and Numerical Contributions to the Aerodynamic Characterization of the IXV Vehicle in High Enthalpy Flow Julien GARRAUD, Onera (France) Inverse Analysis and Identification of Transient Heat Load Distribution on a Reentry Capsule. Toshiya NAKAMURA, JAXA (Japan) TPS - 1 Astriums' TPS Experiments on SHEFEX II Wolfgang P.P. FISCHER, Astrium Space Transportation (Germany) ASTERM : a New Low Density Ablative Material. Jean-Marc BOUILLY, Astrium Space Transportation (France) 15h50-16h20 16h20-16h40 16h40-17h00 17h00-17h20 17h20-17h40 17h40-18h00 AERODYNAMICS - AEROTHERMICS - CFD - 2 Study of Radiating and Ablating Shock Layers Richard MORGAN, University of Queensland (Australia) Radiation in Low Density Hypervelocity Flows. Application to Titan Entry Carolyn JACOBS, Ecole Centrale de Paris (France) Simulation of Shock Tube Radiation Measurements Under Earth Reentry Conditions Adrien LEMAL, Ecole Centrale de Paris (France) A New Computational Technique for Re-entry Flow Calculations Based upon a Shock-fitting Technique for Unstructured Grids Marcello ONOFRI, La Sapienza - University of Rome (Italy) Experimental Investigation of Low Pressure Plasma Flows Focused on Atmospheric Entry Problems Viviana LAGO, ICARE - CNRS (France) GNC AND FLIGHT CONTROL - 2 Shefex III Flight Control System Jürgen TELAAR, Astrium Space Transportation (Germany) On-Line Trajectory Generation and Tracking for Atmospheric Reentry of Reusable Launch Vehicles Daniele ROMAGNOLI, CIRA (Italy) Robustness and Scheduling of the IXV Re-entry Controller Murray KERR, DEIMOS Space S.L.U. (Spain) IXV Avionics Architecture and Development Status Stephane DUSSY, ESA (France) IXV Body Flap Chain Performance Analysis Raffaele AULISIO, Thales Alenia Space (Italy) 20h00-23h00 CONFERENCE DINNER
5 Programme May 28 th, h00-9h30 9h30-10h00 PLENARY INTRODUCTION SESSION Thermal Deformation of Carbon-Carbon Composite Materials during Thermal Cycling under Conditions Simulating the Reentry Trajectory L.L. GRACHEVA, National Acad. Sci. of Ukraine (Ukraine) Construction of Bread Board Model of Non-Ablative Lightweight Thermal Protection System Toshiyuki SUZUKI, Japan Aerospace Exploration Agency (Japan) 10h00-10h30 Catalytic Effects on Hypervelocity Vehicle Valentin BITYURIN, Joint Institute for High Temperatures of Russian Academy of Sciences (Russia) 10h30-11h00 11h00-11h20 11h20-11h40 11h40-12h00 12h00-12h20 MISSION ANALYSIS FAST20XX Achievements and Outlook Rafael MOLINA, European Space Agency (The Netherlands) A Technology Re-entry Vehicle Concept Study Samantha IANELLI, ASI (Italy) Controlled Re-entry from GTO and LEO Feasibility Anne-Hélène GICQUEL, Astrium Satellites (France) Debris Capture System Influence in the Identification of the De-orbiting Policy and Control Laura COSTANZA, AVIOSPACE (Italy) TPS - 2 CMC TPS Technology for IXV: Towards Full-Scale Manufacturing and Qualification Renaud BARRETEAU, Herakles, Safran Group (France) AEROFAST: Development of Innovative Thermal Protections Jean-Marc BOUILLY, Astrium Space Transportation (France) Carbon-phenolic Ablative Materials for Re-entry Space Vehicles: Manufacturing, Properties and Plasma Wind Tunnel (PWT) Test Laura PAGLIA, La Sapienza - University of Rome (Italy) RASTAS SPEAR : Radiation-Shapes- Thermal Protection Investigations for High Speed Earth Re-entry Jean- Marc BOUILLY, Astrium Space Transportation (France) 12h20-14h00 LUNCH 14h00-14h20 AIT Flap Control System (FpCS) for IXV Re-entry Demonstrator Didier VERHOEVEN,SABCA (Belgium) FLIGHT TEST INSTRUMENTATION Destructive Reentry Observing Capsule "i-ball" on HTV3 Yoshihiro KISHINO, IHI Aerospace Co (Japan)
6 May 28 th, h20-14h40 14h40-15h00 15h00-15h20 AIT Development Status of the Body Flap Assembly for the IXV Harald LANGE, MT Aerospace AG (Germany) Design, Justification and Arc Jet Testing of an Optical Window for an Atmospheric Reentry Vehicle Christophe BALEMBOY, Astrium Space Transportation (France) Development of the Nose Cap Attachment for the IXV Re-entry Vehicle Carlos PEREIRA, RUAG Space (Switzerland) FLIGHT TEST INSTRUMENTATION Plasma Effect on Radio-Frequency Communications for Lifting Re-entry Vehicles M.E. D'ELIA, University of Naples "Federico II" (Italy) Measurement of Pressure in the IXV Re-entry Vehicle, Carlos PEREIRA, RUAG Space (Switzerland) The IXV Ground Segment: Design, Architecture, Operational Development and Testing Status Giovanni MARTUCCI, ALTEC S.p.A (Italy) 15h20-15h50 15h50-16h10 SYSTEM DESIGN On a Personal Hypersonic Transportation AirPlane (HyPlane) Valerio CARANDENTE,University of Naples "Federico II" (Italy) 16h10-16h30 «Low energy» Re-entry of Astrium Spaceplane : Unlocking Affordable Suborbital Flights Eugénio FERREIRA, Astrium Space Transportation (France) 16h30-16h50 16h50-17h10 17h10-17h30 Role of Flying Qualities in The IXV Design Process Rodrigo HAYA RAMOS, DEIMOS Space S.L.U. (Spain) A Study of an Unmanned Re-Entry Vehicle with Conventional Landing Capability Mario DE STEFANO FUMO, CIRA (Italy) A Generic Model Driven Approach for Safer Mission and Vehicle Management Software Design Olivier BOUDILLET, Astrium Space Transportation (France) 19h00-20h00 COCKTAIL
7 Programme May 29 th, h00-09h20 DESCENT AND LANDING Building of a Chemical Propulsion System for a Versatile Lander Demonstrator Platform Daniel FIOT, Astrium Space Transportation (France) 09h20-09h40 Preliminary Design Study of EDL System for Japan s Mars Rover Mission Kazuhisa FUJITA, Japan Aerospace Exploration Agency (Japan) 09h40-10h00 10h00-10h20 Multi-disciplinary Design Optimization of an EDL System for High-precision Landing on Mars Bruno CORREIA DA COSTA, Astrium Space Transportation (France) HOMER PROJECT: ILIAD and ODYSSEY GNC Design and Performance Philippe VERNIS, Astrium Space Transportation (France) 10h20-11h00 11h00-11h20 FLIGHT TESTS IXV System Synthesis Drop Test Mock-up Structural Verification Simon APPEL, ESA (France) 11h20-11h40 Qubesat for Aerothermodynamic Research and Measurement on Ablation Gilles BAILET, Von Karman Institute (Belgium) 11h40-12h00 12h00-12h20 Design and Verification Tests of Hayabusa-2 Sample Return Capsule Yamada TETSUYA, Japan Aerospace Exploration Agency (Japan) SHEFEX II, Mission Overview and First Results Hendrik WEIHS, German Aerospace Center DLR (Germany) 12h20-12h30 12h30-14h00 4 TH ARA DAYS CONCLUSION FAREWELL LUNCH
8 GENERAL LOCATION Palais des Congrès d Arcachon Boulevard Veyrier Montagnères Arcachon FRANCE (3/4 hour drive from Bordeaux International Airport) LANGUAGE Papers will be presented in English. Simultaneous translation facilities will not be available. SECRETARIAT All correspondance and inquiries should be sent to the conference secretariat. Avantage Aquitaine 42, rue de Tauzia Bordeaux France Tel/voice box: + 33 (0) Fax: +33 (0) jfb@avantage-aquitaine.com Image : Conception graphique : Sophie Bougnon : sophie.bougnon1@sfr.fr
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