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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

    2013-09-25

    Time

    09:45

    Room

    306B

    IPC members
    • Chairman: Mr. Marc Lacoste, ArianeGroup, France;

    • Chairman: Dr. David E. Glass, National Aeronautics and Space Administration (NASA), United States;

    • Rapporteur: Dr. Luigi Scatteia, PricewaterhouseCoopers Advisory, France;

    papers

    Order

    Time

    Paper title

    Mode

    Presentation status

    Speaker

    Affiliation

    Country

    1

    A competitive thermal protection system for hypersonic vehicles.

    15'

    confirmed

    Dr. Marta Albano

    Sapienza University of Rome

    Italy

    2

    Ablation behaviors of C/C-ZrC-ZrB2-SiC composites by means of arc heated wind tunnel up to 2000?

    15'

    confirmed

    Mr. meng xiangli

    The 4th Academy, China Aerospace Science and Technology Corporation (CASC)

    China

    3

    Catalytic chemical vapor infiltration of carbon nanotube/nanofiber network reinforced carbon/carbon composites: catalytic effect on the densification behavior and matrix microstructure

    15'

    confirmed

    Dr. Hailiang Deng

    Xi'an Aerospace Composites Materials Institute

    China

    4

    Design and Thermal Performance Test of a Novel Thermal Protection/Insulation Antenna Window for Long Time Reentry Space Vehicles

    15'

    Dr. Na Liu

    China Academy of Launch Vehicle Technology (CALT)

    China

    5

    Effect of Preform Structure about Mechanical Properties of Carbon/Carbon Composites

    15'

    confirmed

    Mr. Ying-qiang Liao

    China

    6

    investigation of the thermo-mechanical and ablative behaviour of silicon carbide based concretes exposed to hybrid propulsion environments.

    15'

    confirmed

    Mr. Raffaele D'Elia

    Centre National d'Etudes Spatiales (CNES)

    France

    7

    Investigation on the compressive properties of the 4D in-plane braided C/C composites

    15'

    confirmed

    Mr. Kunlong WEI

    Xi'an institute of aerospace propulsion technology

    China

    8

    Preparation of carbon fiber-reinforced silicon carbide matrix composite by reactive melt infiltration at modest temperature

    15'

    confirmed

    Dr. yanwei zhao

    Aerospace research institute of materials and processing technology (ARIMPT)

    China

    9

    Progressive damage analysis of a 4D in-plane braided C/C composites subjected to unidirectional tension

    15'

    confirmed

    Dr. SHI Hongbin

    Xi'an institute of aerospace propulsion technology

    China

    10

    Research on Thermal Properties of High-performance Carbon Fiber

    15'

    confirmed

    11

    Ablative Material Based On Epoxy Resin Filled With Hollow Glass And Phenolic Resin Microspheres

    15'

    Dr. Carlo Vassalli

    University of Rome “La Sapienza”

    Italy

    12

    The effect of polymerization techniques on the properties of carbon fiber

    15'

    Ms. han xiao

    EMC2

    China

    13

    The relationship between microstructure of SiC coating and tensile strength of CVD-SiC fibers

    15'

    Dr. Song Zhao

    Xi'an Aerospace Composites Institute

    China