session 4

Title: Advanced Materials and Structures for High Temperature Applications
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: 2013-09-25
Time: 09:45
Room: 306B

IPC members

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

papers
Order	Paper title	Selection result	Mode	Presentation status	Speaker	Affiliation	Country
1	A competitive thermal protection system for hypersonic vehicles.	accepted	15'	confirmed	Dr. Marta Albano	Sapienza University of Rome	Italy
2	Ablation behaviors of C/C-ZrC-ZrB2-SiC composites by means of arc heated wind tunnel up to 2000?	accepted	15'	confirmed	Mr. meng xiangli	The 4th Academy, China Aerospace Science and Technology Corporation (CASC)	China
3	Catalytic chemical vapor infiltration of carbon nanotube/nanofiber network reinforced carbon/carbon composites: catalytic effect on the densification behavior and matrix microstructure	accepted	15'	confirmed	Dr. Hailiang Deng	Xi'an Aerospace Composites Materials Institute	China
4	Design and Thermal Performance Test of a Novel Thermal Protection/Insulation Antenna Window for Long Time Reentry Space Vehicles	accepted	15'		Dr. Na Liu	China Academy of Launch Vehicle Technology (CALT)	China
5	Effect of Preform Structure about Mechanical Properties of Carbon/Carbon Composites	accepted	15'	confirmed	Mr. Ying-qiang Liao		China
6	investigation of the thermo-mechanical and ablative behaviour of silicon carbide based concretes exposed to hybrid propulsion environments.	accepted	15'	confirmed	Mr. Raffaele D'Elia	Centre National d'Etudes Spatiales (CNES)	France
7	Investigation on the compressive properties of the 4D in-plane braided C/C composites	accepted	15'	confirmed	Mr. Kunlong WEI	Xi'an institute of aerospace propulsion technology	China
8	Preparation of carbon fiber-reinforced silicon carbide matrix composite by reactive melt infiltration at modest temperature	accepted	15'	confirmed	Dr. yanwei zhao	Aerospace research institute of materials and processing technology (ARIMPT)	China
9	Progressive damage analysis of a 4D in-plane braided C/C composites subjected to unidirectional tension	accepted	15'	confirmed	Dr. SHI Hongbin	Xi'an institute of aerospace propulsion technology	China
10	Research on Thermal Properties of High-performance Carbon Fiber	accepted	15'	confirmed
11	Ablative Material Based On Epoxy Resin Filled With Hollow Glass And Phenolic Resin Microspheres	accepted	15'		Dr. Carlo Vassalli	University of Rome “La Sapienza”	Italy
12	The effect of polymerization techniques on the properties of carbon fiber	accepted	15'		Ms. han xiao	EMC2	China
13	The relationship between microstructure of SiC coating and tensile strength of CVD-SiC fibers	accepted	15'		Dr. Song Zhao	Xi'an Aerospace Composites Institute	China

session 4

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