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  • 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

    2018-10-03

    Time

    09:45

    Room

    ÖVB 2

    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. Zijun Hu, China Academy of Launch Vehicle Technology (CALT), China;

    papers

    Order

    Time

    Paper title

    Mode

    Presentation status

    Speaker

    Affiliation

    Country

    1

    KEYNOTE: Santini Lecture, given by Gerben Sinnema: Safety of spaceflight structures - The application of fracture and damage control

    30

    confirmed

    Mr. Gerben Sinnema

    European Space Agency (ESA-ESTEC)

    The Netherlands

    2

    Aerodynamic Heating Research of Scramjet Inlet Through the Duplicating Hypersonic Flight Condition Wind Tunnel

    12

    Dr. Zhaowei Wang

    China Academy of Launch Vehicle Technology (CALT)

    China

    3

    Architectured Ceramics with Improved Toughness for High Temperature Applications

    12

    confirmed

    Dr. Behnam Ashrafi

    National Research Council

    Canada

    4

    Characterization of Carbon-Fiber Reinforced Ultra-High-Temperature Ceramic Matrix Composites in Arc-jet Environment

    12

    confirmed

    Mr. Stefano Mungiguerra

    Università degli Studi di Napoli “Federico II”

    Italy

    5

    Investigation of Passive to Active Oxidation Transition on Ultra High Temperature Ceramics

    12

    confirmed

    Mr. Daniel Galla

    IRS, University of Stuttgart

    Germany

    6

    Multi-dimensional coupled approach for the simulation of ablative thermal protection systems during atmospheric entries.

    12

    withdrawn

    Ms. Viola Renato

    Univeristy of Strathclyde

    United Kingdom

    7

    Analysis and test results on heat insulation performance of lightweight thermal protection structure

    12

    confirmed

    Mr. CHEN XUAN

    Science and Technology on Space Physics Laboratory

    China

    8

    oxidation and heterogeneous catalysis on titanium Ti-6Al-4V in high-enthalpy flows

    12

    confirmed

    Mr. Bartomeu Massuti Ballester

    IRS, University of Stuttgart

    Germany

    9

    Properties of carbon reinforced polybenzoxazine resin composites – an ablative material with new structure

    12

    confirmed

    Prof.Dr. Yalin Guo

    Xi'an Aerospace Composites Research Institute

    China

    10

    optimal design of thermal protection considering the carbon foam morphology

    12

    confirmed

    Prof. Oleg Alifanov

    Moscow Aviation Institute

    Russian Federation

    11

    Study on mechanical behavior of C/SiC structure under high temperature based on acoustic emission analysis

    12

    withdrawn

    Dr. Denghong Xiao

    Beijing Electro-Mechanical Engineering Institute, China Aerospace Science & Industry Corporation (CASIC)

    China