session 4

Title: Advanced Materials and Structures for High Temperature Applications
type: oral
Description: The topics to be addressed include advanced materials and structures for high temperature applications in space related domains. This includes carbon-carbon and ceramic matrix composites, ultra high temperature ceramics, ablative materials, ceramic tiles and insulations, together with innovative structural concepts making use of the above, for propulsion systems, launchers, hypersonic vehicles, entry vehicles, aero capture, power generation. The session covers the full spectrum of material, design, manufacturing and testing aspects.
Date: 2014-10-01
Time: 09:45
Room: 713A

IPC members

Co-Chair: Mr. Marc Lacoste, ArianeGroup, France;
Co-Chair: Dr. David E. Glass, National Aeronautics and Space Administration (NASA), United States;
Rapporteur: Dr. Luigi Scatteia, PricewaterhouseCoopers Advisory (PwC), France;

papers
Order	Paper title	Mode	Presentation status	Speaker	Affiliation	Country
1	Emissivity Analyses Of Materials Candidate For Eart’s Atmosphere Re-Entry From Space Missions	12'	confirmed	Dr. Carlo Purpura	CIRA Italian Aerospace Research Centre	Italy
2	estimation of surface heat flux for ablation and charring of thermal protection material	12'	no-show	Dr. Weiqi Qian	China Aerodynamics Research and Developement Center	China
3	Plasma Wind Tunnel Tests for C/SiC Composite with Additional Mechanical Tensile Load	12'	no-show	Mr. dongbin ou	China Academy of Aerospace Aerodynamics (CAAA)	China
4	Dynamic response testing and analysis of hypersonic aircraft panels excited by high-intensity acoustic loads in thermal environment	12'	no-show	Mr. Zhenqiang Wu	Beijing Institute of Structure and Environment Engineering	China
5	A new type scramjet thermal protection structure based on high temperature heat pipe technique	12'	confirmed	Prof.Dr. Ai Bangcheng	China Academy of Aerospace Aerodynamics (CAAA)	China
7	design study on multi-layered stand-off thermal protection system using porous titanium sandwich panels	12'	confirmed	Mr. Ryosuke Hayashi	Waseda University	Japan
8	A New Reusable Thermal Protection System Concept for Earth Atmospheric Re-Entry	12'	withdrawn	Dr. Jorge Barcena	Tecnalia Research and Innovation	Spain
9	Hybrid Ablative/Ceramic Thermal Protection System: Mission Profile, Materials Selection, Interface Development and Verification Approach	12'	withdrawn	Dr. Jorge Barcena	Tecnalia Research and Innovation	Spain
10	A Comparative Assessment of Criticality of Local Damage in Composite Liner of a Nozzle Through Finite Element Thermal-Structural Analysis	12'	confirmed	Mr. Thomas Kurian	Indian Space Research Organization (ISRO)	India
11	Thermally and Dimensionally Stable Structures of Carbon-Carbon Laminated Composites for Space Applications	12'	no-show	Dr. Volodymyr Slyvynskyi	“NIKE” Ltd. Scientific and Production Enterprise	Ukraine
12	The Ablative Performance of Light Weight Charring Ablators in High Enthalpy Environment	12'	no-show	Dr. HE GAO	China Academy of Aerospace Aerodynamics (CAAA)	China
13	Heat Pipe Cooled Leading Edges	12'	withdrawn	Dr. Suraj Rawal	Lockheed Martin Space Systems Company	United States

session 4

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