Novel Hybrid Ablative/Ceramic Development for Re-Entry in Planetary Atmospheric Thermal Protection: Interfacial Adhesive Selection and Test Verification Plan: Interfacial adhesive selection and test verification plan

Jorge Barcena, Sonia Florez, Beatriz Perez, Jean-Marc Bouilly, Gregory Pinaud, Wolfgang P. Fischer, Agnes de Montbrun, Michel Descomps, Christian Zuber, Waldermar Rotaermel, Ing Hermann Hald, Pedro Portela, Konstantina Mergia, Kostoula Triantou, George Vekinis, Adriana Stefan, Cristina Ban, Gheorghe Ionescu, Dominique Bernard, Vincent LeroyBartomeu Massuti, Georg H. Herdrich, A. Marinou, T. Massuti

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9 Citas (Scopus)

Resumen

The FP7 project HYDRA addresses the development of a hybrid thermal protection solution, where a low density ablator is attached on top of a thermo-structural ceramic core by means of the use of high temperature adhesives. The project aims to design, integrate and verify a robust and lightweight thermal shield solution for atmospheric earth re-entry. The main advantage of a hybrid heat-shield is based on the capability of the thin ablative top layer to bear high thermal loads, while the tough ceramic composite underneath provides structural support.
Idioma originalInglés
Título de la publicación alojadaunknown
EditorialAIAA American Institute of Aeronautics and Astronautics
ISBN (versión impresa)9781624102844
DOI
EstadoPublicada - 2014
EventoAIAA AVIATION 2014 -19th AIAA International Space Planes and Hypersonic Systems and Technologies Conference 2014 - Atlanta, GA, Estados Unidos
Duración: 16 jun 201420 jun 2014

Serie de la publicación

NombreAIAA AVIATION 2014 -19th AIAA International Space Planes and Hypersonic Systems and Technologies Conference

Conferencia

ConferenciaAIAA AVIATION 2014 -19th AIAA International Space Planes and Hypersonic Systems and Technologies Conference 2014
País/TerritorioEstados Unidos
CiudadAtlanta, GA
Período16/06/1420/06/14

Palabras clave

  • Thermal Protection Systems
  • Atmospheric Re-entry
  • Ablative materials
  • Ceramic Matrix Composites

Project and Funding Information

  • Project ID
  • info:eu-repo/grantAgreement/EC/FP7/283797/EU/Hybrid Ablative Development for Re-Entry in Planetary Atmospheric Thermal Protection/HYDRA
  • Funding Info
  • European Commission FP7, 283797, HYDRA

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