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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

    2023-10-04

    Time

    10:15

    Room

    BCC A1

    IPC members
    • Co-Chair: Dr. David E. Glass, National Aeronautics and Space Administration (NASA), United States;

    • Co-Chair: Mr. Thierry Pichon, ArianeGroup, France;

    papers

    Order

    Time

    Paper title

    Mode

    Presentation status

    Speaker

    Affiliation

    Country

    1

    10:15

    Design of a novel integrated structure considering heat-transport and load-bearing capacities for hypersonic vehicles

    12

    confirmed

    Dr. Jian-Jun Gou

    Northwestern Polytechnical University

    China

    2

    10:27

    Heat-resistant MoSi2 – NbSi2 and Cr-Ni coatings for rocket engine combustion chambers and respective vacuum-arc deposition technology

    12

    confirmed

    Dr. Volodymyr Nadtoka

    Yuzhnoye State Design Office

    Ukraine

    3

    10:39

    Thermal stability of polymer derived ultra-high temperature ceramic matrix composites

    12

    confirmed

    Dr. Luca Zoli

    CNR - ISSMC

    Italy

    4

    10:51

    Anisotropic Composite Heat-Shielding Materials based on Glassy Carbon and Pyrolytic Graphite: Analyzing Effectiveness in case of a Re-entry Module of a Lunar Probe

    12

    confirmed

    Dr. Victor Leonov

    Bauman Moscow State Technical University

    Russian Federation

    5

    11:03

    Processing and testing of UHTCMCs for aerospace applications

    12

    confirmed

    Dr. Diletta Sciti

    CNR - ISSMC

    Italy

    6

    11:15

    The importance of using thermal barrier coatings in aero gas turbine engines. Ceramic materials for thermal barrier coatings: A review and current status

    12

    confirmed

    Mr. Ibrahim Muradzade

    National Aviation Academy - Azerbaijan

    Azerbaijan

    7

    11:27

    Unleashing the Potential of Ceramic Matrix Composites for Hypersonic Flight

    12

    confirmed

    Mr. Joyjit Barua

    Concordia University

    Canada

    8

    11:39

    ZrO2 reinforced ablative material suitable for the thermal protection system of ultra-high temperature in solid rocket motor combustion chamber

    12

    confirmed

    Dr. MengFei Guo

    China

    9

    11:51

    Challenges and Solutions for High-Temperature Applications in Space: Materials and Structures for Spacecraft and Satellites"

    12

    confirmed

    Mr. Mohammed Umar

    R.V.College of Engineering

    India

    10

    12:03

    heat transfer analysis for an ablative combustion chamber: insights & methodologies

    12

    withdrawn

    Mr. Intisar Salam

    Concordia University

    Canada

    11

    12:15

    Design of thermal protection based on carbon aerogel composite structure optimization

    12

    confirmed

    Ms. Margarita Salosina

    Moscow Aviation Institute (National Research University)

    Russian Federation