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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

    2022-09-20

    Time

    10:15

    Room

    W06

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

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

    • Rapporteur: Dr. Zijun Hu, China Academy of Launch Vehicle Technology (CALT), China;

    papers

    Order

    Time

    Paper title

    Mode

    Presentation status

    Speaker

    Affiliation

    Country

    1

    10:15

    KEYNOTE: Paolo Santini's Memorial Lecture - Active damping, vibration isolation and shape control of space structures

    30

    confirmed

    Prof. André Preumont

    University of Brussels

    Belgium

    2

    10:45

    a novel thermal protection system via opposing jet arrays for reusable reentry vehicles

    11

    confirmed

    Dr. Xiaoyan Li

    CASC

    China

    3

    10:56

    In-situ emissivity assessment of grade 5 titanium in high-enthalpy flows for catalysis investigations

    11

    confirmed

    Mr. Clemens Felix Kaiser

    University of Stuttgart

    Germany

    4

    11:07

    Innovative superalloy powder designed for Additive Manufacturing and for high temperature use up to 900°C

    11

    confirmed

    Mrs. Solange Vivès

    Aubert & Duval

    France

    5

    11:18

    Preliminary design of the heat shield for a Mars entry vehicle

    11

    withdrawn

    Mr. Gianmarco Floro

    Politecnico di Torino

    Italy

    6

    11:29

    Thermo structural analysis and test results of solid rocket motor submerged Nozzle throat with 4-D Carbon-Carbon (C-C) and graphite material

    11

    confirmed

    Mr. Paul Murugan J

    Vikram Sarabhai Space Centre, ISRO, Thiruvananthapuram

    India

    7

    11:40

    performance enhancement of cooler micro-vibration isolation system by implementing thermal design with graphite sheet

    11

    confirmed

    Ms. Hye-In Kim

    Chosun University

    Korea, Republic of

    8

    11:51

    Design of thermal protection based on carbon aerogel composite with optimal structure

    11

    confirmed

    Ms. Margarita Salosina

    Moscow Aviation Institute (National Research University)

    Russian Federation

    9

    12:02

    Development of the analysis methods for Solar probe thermal protection

    11

    confirmed

    Dr. Alena V. Morzhukhina

    Moscow Aviation Institute (National Research University, MAI)

    Russian Federation

    10

    12:13

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

    11

    confirmed

    Dr. Victor Leonov

    Bauman Moscow State Technical University

    Russian Federation

    11

    12:24

    Improvements in PI Aerogels for Flexible Thermal Protection System - Hypersonic Inflatable Aerodynamic Decelerator (HIAD)

    11

    confirmed

    Mr. Tushar Agarwal

    Sardar Vallabhbhai National Institute of Technology Surat

    India

    12

    12:35

    Space Rider: Thermal Protection System and Control Surfaces design, development and qualification status

    11

    confirmed

    Dr. Giuseppe Rufolo

    CIRA Italian Aerospace Research Centre

    Italy