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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

    2016-09-28

    Time

    09:45

    Room

    Salon de Eventos 1

    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

    Design and Qualification of Aft Bay Thermal Protection System of KSLV-II

    15'

    withdrawn

    Dr. JONGMIN KIM

    Korea Aerospace Research Institute (KARI)

    Korea, Republic of

    2

    Carbon / Carbon high thickness shell for hypersonic vehicles.

    15'

    confirmed

    Dr. Marta Albano

    Agenzia Spaziale Italiana (ASI)

    Italy

    3

    Advanced Silica Tile Thermal Protection System for Reusable Launch Vehicles: Development & Qualification

    15'

    no-show

    4

    Currently performed Research and Development activities in the field of Atmospheric Entry at IRS

    15'

    no-show

    Prof.Dr. Georg Herdrich

    Institute of Space Systems

    Germany

    5

    Improvement and qualification of a plasma wind-tunnel to CO2 flows for Mars entry testing

    15'

    confirmed

    Prof. Christian Mundt

    Universität der Bundeswehr München

    Germany

    6

    The Study of a 4D Radial-rod Low Erosion Fine Woven C/C Composite

    15'

    no-show

    Mrs. Li ya-di

    China

    7

    Investigation on the ablation performance of EPDM insulation material under dense particle stream

    15'

    confirmed

    Dr. Tuanwei XU

    The xi'an institute of aerospace propulsion technology

    China

    8

    Simulation of Acoustic Emission Wave Propagation in Thermal Protection System with Plain Weave C/SiC Composite

    15'

    no-show

    Dr. Denghong Xiao

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

    China

    9

    Effect of interfacial properties on nonlinear behavior of the 4D in-plane braided C/C composites

    15'

    confirmed

    Dr. Kunlong WEI

    Xi'an institute of aerospace propulsion technology

    China

    10

    Finite volume method for modeling the thermal environment to carry out thermal protection structure coupling analysis

    15'

    confirmed

    Mr. XIANG ZHANG

    China Academy of Launch Vehicle Technology(CALT)

    China

    11

    based on the minimum energy principle prediction of crack spacing and depth of ceramics under thermal shock

    15'

    confirmed

    Mr. tao yongqiang

    China