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  • 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

    2015-10-14

    Time

    09:45

    Room

    Oranim 1 (ICC, lower level)

    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

    5th Paolo Santini Memorial Lecture: Inverse Methods in Identification and Modeling of Thermal Processes in Aerospace Materials and Structures: Theory and Practice

    30'

    confirmed

    Prof. Oleg Alifanov

    Moscow Aviation Institute

    Russian Federation

    2

    Role of effective ablative materials in the heat shield of rockets

    15'

    no-show

    Ms. Shridutta Banerjee

    India

    3

    Predicting methods of high temperature performance for Reusable Launch Vehicle thermal protection materials

    15'

    confirmed

    Mr. Ai Bang cheng

    China

    4

    Properties of Carbon and SiC foam as thermal insulator for space thermal protection systems.

    12'

    confirmed

    Dr. Marta Albano

    Sapienza University of Rome

    Italy

    5

    properties of C/C-SiC composites used as space materials

    15'

    no-show

    Mr. Kunjie Wang

    Xi'an Aerospace Composites Research Institute

    China

    6

    Thermo-chemical Ablation Mechanism of EPDM Internal Insulator

    15'

    confirmed

    Ms. Wenli Wang

    China

    7

    Thermo-chemical Ablation Characteristics of Silicone Rubber Based Insulator

    15'

    withdrawn

    Prof. Wei Zhang

    National University of Defense Technology

    China

    8

    University of Kentucky Plasma Diagnostic Facilities for the Investigation of Gas-Surface Interactions

    15'

    confirmed

    Mr. Bradley Butler

    University of Kentucky

    United States