%0 Journal Article 
%A Barcena, Jorge
%A Florez, Sonia
%A Perez, Beatriz
%A Bouilly, Jean-Marc
%A Pinaud, Gregory
%A Fischer, Wolfgang P.
%A de Montbrun, Agnes
%A Descomps, Michel
%A Zuber, Christian
%A Rotaermel, Waldermar
%A Hermann Hald, Ing
%A Portela, Pedro
%A Mergia, Konstantina
%A Triantou, Kostoula
%A Vekinis, George
%A Stefan, Adriana
%A Ban, Cristina
%A Ionescu, Gheorghe
%A Bernard, Dominique
%A Leroy, Vincent
%A Massuti, Bartomeu
%A Herdrich, Georg H.
%T Novel Hybrid Ablative/Ceramic Development for Re-Entry in Planetary Atmospheric Thermal Protection: Interfacial Adhesive Selection and Test Verification Plan
%D 2014
* AIAA American Institute of Aeronautics and Astronautics
%X 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.
%K Thermal Protection Systems
%K Atmospheric Re-entry
%K Ablative materials
%K Ceramic Matrix Composites
doi 10.2514/6.2014-2373
%U http://hdl.handle.net/11556/380
%~ GOEDOC, SUB GOETTINGEN