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  • IAC-23
  • C2
  • session 4
  • 4. Advanced Materials and Structures for High Temperature Applications

    Papers

    1. Design of a novel integrated structure considering heat-transport and load-bearing capacities for hypersonic vehicles

    2. Heat-resistant MoSi2 – NbSi2 and Cr-Ni coatings for rocket engine combustion chambers and respective vacuum-arc deposition technology

    3. Thermal stability of polymer derived ultra-high temperature ceramic matrix composites

    4. Anisotropic Composite Heat-Shielding Materials based on Glassy Carbon and Pyrolytic Graphite: Analyzing Effectiveness in case of a Re-entry Module of a Lunar Probe

    5. Processing and testing of UHTCMCs for aerospace applications

    6. The importance of using thermal barrier coatings in aero gas turbine engines. Ceramic materials for thermal barrier coatings: A review and current status

    7. Unleashing the Potential of Ceramic Matrix Composites for Hypersonic Flight

    8. ZrO2 reinforced ablative material suitable for the thermal protection system of ultra-high temperature in solid rocket motor combustion chamber

    9. Challenges and Solutions for High-Temperature Applications in Space: Materials and Structures for Spacecraft and Satellites"

    11. Design of thermal protection based on carbon aerogel composite structure optimization