• Home
  • IAF Digital Library
  • Public Website
  • My papers
  • Home
  • event
  • IAC-17
  • C2
  • 4
  • 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

    2017-09-27

    Time

    09:45

    Room

    Panorama Room 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: Paolo Santini Memorial Lecture Materials and Structures Technology insertion into Spacecraft Systems: Successes and Challenges

    30

    confirmed

    Dr. Suraj Rawal

    Lockheed Martin Space Systems Company

    United States

    2

    Systematic Comparative Analysis of Existing Ablative Materials for Thermal Protection Systems’ Design Optimisation

    12

    confirmed

    Mr. Francesco Romano

    Institute of Space Systems, University of Stuttgart

    Germany

    3

    Microstructures and ablation behaviors of carbon/carbon composites under aggressive ablation environments in a solid rocket motor

    12

    confirmed

    Prof.Dr. Li Qiang

    Northwestern Polytechnical University

    China

    4

    Mechanical and ablative properties of C/C composites modified by SiC using liquid silicon infiltration method

    12

    confirmed

    Mr. JinHuang Zheng

    China

    5

    Thermal response and recession resistance of a new thermal protection system using high-temperature CFRP sandwich panel

    12

    confirmed

    Mr. Ousei Miyamoto

    Waseda University

    Japan

    6

    Multi-dimensional Ablation and Thermal Response Program for Re-entry Analysis

    12

    confirmed

    Ms. Viola Renato

    Univeristy of Strathclyde

    United Kingdom

    7

    REVIEW ON LIGHTWEIGHT GRADED NON-ABLATION STRUCTURE FOR HYPERSONIC VEHICLES

    12

    confirmed

    Dr. qin lu

    CAAA

    China

    8

    Design and Thermo-Structural analysis of the interface between subscale version of Carbon-Carbon (C-C) Nozzle divergent to metallic flange hardware for a ground simulation test

    12

    confirmed

    Mr. Paul Murugan J

    Indian Space Research Organization (ISRO)

    India

    9

    Experimental Investigation of the Emissivity of UHTC Coatings on CMC Materials in GHIBLI Plasma Wind Tunnel Tests

    12

    confirmed

    Dr. Carlo Purpura

    CIRA Italian Aerospace Research Centre

    Italy

    10

    IRS Research and Development activities in the field of Atmospheric Entry

    12

    confirmed

    Prof.Dr. Georg Herdrich

    Institute of Space Systems

    Germany

    11

    Fabrication and Validation Test of a Novel Thermal Protection Structure Based on Heat Pipe Technology for Combustion Chamber of Scramjet

    12

    confirmed

    Prof.Dr. Ai Bangcheng

    China Academy of Aerospace Aerodynamics (CAAA)

    China