Paper information

Paper code

IAC-14,C2,4,9,x25745

Order

9

Room

713A

Title

Hybrid Ablative/Ceramic Thermal Protection System: Mission Profile, Materials Selection, Interface Development and Verification Approach

abstract

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Session

4. Advanced Materials and Structures for High Temperature Applications

symposium

C2. MATERIALS AND STRUCTURES SYMPOSIUM

congress

IAC-14

Type of presentation

oral

Main author

Dr. Jorge Barcena, Tecnalia Research and Innovation, Spain

Co-authors

Dr. Sonia Florez, Tecnalia Research and Innovation, Spain;

Mrs. Beatriz Perez, Tecnalia Research and Innovation, Spain;

Mr. Gregory Pinaud, Airbus Defence & Space, France;

Dr. Jean Marc Bouilly, Airbus Defence & Space, France;

Mr. Wolfgang P.P. Fischer, Airbus Defence & Space, Germany;

Mrs. Agnes de Montbrun, Lièges HPK SA, France;

Mr. Christian Zuber, Deutsches Zentrum für Luft- und Raumfahrt, Germany;

Mr. Waldermar Rotaermel, Deutsches Zentrum für Luft- und Raumfahrt e.V. (DLR), Germany;

Dr. Hermann Hald, Deutsches Zentrum für Luft- und Raumfahrt e.V. (DLR), Germany;

Dr. Celeste Pereira, Hps-high Performance Structures, Lda, Portugal;

Mr. Joao Pedro Loureiro, Hps-high Performance Structures, Lda, Portugal;

Dr. Konstantina Mergia, National Center For Scientific Research (Ncsr) "Demokritos", Greece;

Dr. Kostoula Triantou, National Center For Scientific Research (Ncsr) "Demokritos", Greece;

Dr. Giorgios Vekinis, National Center For Scientific Research (Ncsr) "Demokritos", Greece;

Mrs. Cristina Ban, National Institute for Aerospace Research Bucharest (INCAS), Romania;

Dr. Adriana Stefan, National Institute for Aerospace Research Bucharest (INCAS), Romania;

Dr. Vincent Leroy, CNRS-ICMCB, France;

Dr. Dominique Benard, CNRS-ICMCB, France;

Mr. Bartomeu Massuti Ballester, IRS, University of Stuttgart, Germany;

Prof.Dr. Georg Herdrich, Institute of Space Systems, Germany;