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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

    2019-10-23

    Time

    09:45

    Room

    152B

    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

    09:45

    KEYNOTE: Paolo Santini's Memorial Lecture: Ablators from Apollo to Future Missions to Moon, Mars, and Beyond

    24

    confirmed

    Dr. Ethiraj Venkatapathy

    NASA Ames Research Center

    United States

    2

    10:09

    Designing Building and Testing of a Thermal Protection System for a Spacecraft Which Cannot be Qualified Using the Standard Methodology

    12

    confirmed

    Mr. edward schaefer

    JHU Applied Physics Laboratory

    United States

    3

    10:21

    Parker Solar Probe Structural-Thermal Analysis Challenges

    12

    confirmed

    Mrs. Shelly Conkey

    JHU Applied Physics Laboratory

    United States

    4

    10:33

    Effect of SiC concentration on aero-thermo-dynamic behavior of ZrB2-based ceramics in hypersonic environment

    12

    confirmed

    Mr. Stefano Mungiguerra

    Università degli Studi di Napoli “Federico II”

    Italy

    5

    10:45

    Design and experimental analysis of a three-segment sandwich structure nose cone for hypersonic vehicle with a compare study of numerical simulation experimental method

    18

    confirmed

    Mr. XIANG ZHANG

    China Academy of Launch Vehicle Technology(CALT)

    China

    6

    11:03

    Design and experimental verification research of a convenient high temperature resistance self-lubricating CMC hinge for control surface of hypersonic vehicle

    18

    confirmed

    Mr. XIANG ZHANG

    China Academy of Launch Vehicle Technology(CALT)

    China

    7

    11:21

    Structural Design and Analysis of an Aeroshell for a Human crew Re-entry Vehicle

    12

    confirmed

    Mr. Rohan Chandra

    University of Petroleum and Energy Studies

    India

    8

    11:33

    Protective heat resistant coating for Inconel 718 additively manufactured parts

    12

    confirmed

    Mrs. Elena Karasik

    Firefly Aerospace Inc.

    Ukraine

    9

    11:45

    Extreme-Temperature Carbon- and Ceramic-Matrix Composite Nozzle Extensions for Liquid Rocket Engines

    12

    confirmed

    Mr. Peter Valentine

    National Aeronautics and Space Administration (NASA)

    United States

    10

    11:57

    C/C-SiC CERAMIC MATRIX COMPOSITE ORBITAL THRUSTER DEVELOPMENT FOR HPGP OPERATION

    12

    confirmed

    Mr. Ilja Mueller

    German Aerospace Center (DLR)

    Germany

    11

    12:09

    Method of heat-proof nickel alloys mechanical properties improvement for rocket engines

    12

    confirmed

    Ms. Maryna Hrekova

    Yuzhnoye State Design Office

    Ukraine

    12

    12:21

    An active and passive combined thermal protection technology for flow distribution in parallel channels

    12

    confirmed

    Mr. Chen Siyuan

    China Academy of Aerospace Aerodynamics (CAAA)

    China