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  • session 5

    Title

    Space Structures and Materials for Extreme Environment (High-temperature and cryogenic-temperature applications including thermal insulation concepts)

    Description

    The topics to be addressed include structures and materials for extreme environments, including both cryogenic applications and high temperature applications in space related domains. The session covers the full spectrum of material, design, manufacturing and testing. Operation of structures and mechanisms in cryogenic environment is quite challenging. This concerns the components design as well as the materials they are made of or lubricants needed for proper functioning. Tanks for storage of cryogenic propellants for launch vehicle application or long term storage of cryogenic liquids require an appropriate material selection and characterization, especially when organic composite materials are considered. Cryogenic insulation for propellant tanks and lines, especially for reusable launch vehicles exposed to aerothermal loads might require a combination with high temperature thermal protection systems. (Foam with metallic protection, vacuum insulated sandwich, stand-off thermal protection…). For the elevated temperature regime, this session includes carbon-carbon and ceramic matrix composites, ultra-high temperature ceramic matrix composites, ablative materials, ceramic tiles and insulations, together with innovative structural concepts making use of the above, for propulsion systems, launchers, hypersonic vehicles, re-entry vehicles, aero capture, power generation.

    Date

    2024-10-16

    Time

    15:00

    Room

    Orange Hall 1

    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;

    • Rapporteur: Mr. James Tucker, [unlisted], United States;

    papers

    Order

    Time

    Paper title

    Mode

    Presentation status

    Speaker

    Affiliation

    Country

    1

    15:00

    KEYNOTE: PAOLO SANTINI MEMORIAL LECTURE - In Space Manufacturing and Extraterrestrial Construction - How Did We Get Here? - Where Are We? - Where Should We Be Going? - THE CHALLENGE: Will We Be Ready?

    40

    confirmed

    Dr. Raymond G. Clinton

    NASA Marshall Space Flight Center

    United States

    2

    15:40

    Advanced Oxide Ceramic Matrix Composite Inlet with Deployable Flap for Re-Entry Environments

    10

    confirmed

    Ms. Valerie L. C. Dosch

    Walter E.C. Pritzkow Spezialkeramik

    Germany

    3

    15:50

    multi-plateau auxetic metamaterials constructed by intracellular and intercellular gradients for energy absorption in space

    10

    confirmed

    Dr. Changfang Zhao

    Tsinghua University

    China

    4

    16:00

    material characterization and plasma testing for an inflatable heatshield for the EARS reusable smallsat platform

    10

    confirmed

    Mr. Simone Del Monte

    von Karman Institute for Fluid Dynamics

    Belgium

    5

    16:10

    The Aurora Configuration of SCIROCCO Plasma Wind Tunnel for Experiments at Super-Orbital Re-Entry Conditions

    10

    confirmed

    Mr. Eduardo Trifoni

    Australian National University (ANU)

    Australia

    6

    16:20

    Metamaterial Design and Manufacturing Technologies for Extreme Environment Applications

    10

    confirmed

    Prof. Pengfei Wang

    China Academy of Aerospace Science and Innovation

    China

    7

    16:30

    The fatigue performance study of a leading edge under high temperature

    10

    confirmed

    Dr. Liqiang Ai

    China Academy of Launch Vehicle Technology (CALT)

    China

    8

    16:40

    Multilayer Anisotropic Heat Shield: Analysis of the Structure and Thermal Stress State in Case of a Lunar Probe Re-entry Module

    10

    confirmed

    Dr. Victor Leonov

    Bauman Moscow State Technical University

    Russian Federation

    9

    16:50

    Thermal Shielding Concepts for Cryogenic Superconducting Magnets and Plasma Propulsion Systems

    10

    confirmed

    Mr. Randy Pollock

    Victoria University of Wellington

    New Zealand

    10

    17:00

    Joining of C/C-SiC ceramic matrix composites to high-entropy alloys using cobalt-based fillers for in-space applications

    10

    confirmed

    Mrs. Ebrar Ekiz

    ARCEON B.V.

    The Netherlands

    11

    17:10

    Experimental Testing and Enhanced Modelling of CMC and UHTCMC Materials for Extreme Environments

    10

    withdrawn

    Dr. Mario De Stefano Fumo

    CIRA Italian Aerospace Research Center, Capua

    Italy

    *

    Numerical and experimental approach for the design of CMC and UHTCMC reusable structures: results of AM3aC2A project

    10

    Prof. ALESSANDRO AIROLDI

    Politecnico di Milano

    Italy

    *

    Thermal Transient Analysis for Non-Destructive Thermography in Damaged Composites Using Carrera Unified Formulation

    10

    confirmed

    Ms. Sidra Riaz

    Politecnico di Bari

    Italy