TY - GEN
T1 - Novel Hybrid Ablative/Ceramic Development for Re-Entry in Planetary Atmospheric Thermal Protection: Interfacial Adhesive Selection and Test Verification Plan
T2 - AIAA AVIATION 2014 -19th AIAA International Space Planes and Hypersonic Systems and Technologies Conference 2014
AU - Barcena, Jorge
AU - Florez, Sonia
AU - Perez, Beatriz
AU - Bouilly, Jean-Marc
AU - Pinaud, Gregory
AU - Fischer, Wolfgang P.
AU - de Montbrun, Agnes
AU - Descomps, Michel
AU - Zuber, Christian
AU - Rotaermel, Waldermar
AU - Hermann Hald, Ing
AU - Portela, Pedro
AU - Mergia, Konstantina
AU - Triantou, Kostoula
AU - Vekinis, George
AU - Stefan, Adriana
AU - Ban, Cristina
AU - Ionescu, Gheorghe
AU - Bernard, Dominique
AU - Leroy, Vincent
AU - Massuti, Bartomeu
AU - Herdrich, Georg H.
AU - Marinou, A.
AU - Massuti, T.
PY - 2014
Y1 - 2014
N2 - 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.
AB - 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.
KW - Thermal Protection Systems
KW - Atmospheric Re-entry
KW - Ablative materials
KW - Ceramic Matrix Composites
KW - Thermal Protection Systems
KW - Atmospheric Re-entry
KW - Ablative materials
KW - Ceramic Matrix Composites
UR - http://www.scopus.com/inward/record.url?scp=85085773150&partnerID=8YFLogxK
U2 - 10.2514/6.2014-2373
DO - 10.2514/6.2014-2373
M3 - Conference contribution
SN - 9781624102844
T3 - AIAA AVIATION 2014 -19th AIAA International Space Planes and Hypersonic Systems and Technologies Conference
BT - unknown
PB - AIAA American Institute of Aeronautics and Astronautics
Y2 - 16 June 2014 through 20 June 2014
ER -