rootbrowseIAC-23C2session 44. Advanced Materials and Structures for High Temperature ApplicationsPapers1. Design of a novel integrated structure considering heat-transport and load-bearing capacities for hypersonic vehicles2. Heat-resistant MoSi2 – NbSi2 and Cr-Ni coatings for rocket engine combustion chambers and respective vacuum-arc deposition technology3. Thermal stability of polymer derived ultra-high temperature ceramic matrix composites4. Anisotropic Composite Heat-Shielding Materials based on Glassy Carbon and Pyrolytic Graphite: Analyzing Effectiveness in case of a Re-entry Module of a Lunar Probe5. Processing and testing of UHTCMCs for aerospace applications6. The importance of using thermal barrier coatings in aero gas turbine engines. Ceramic materials for thermal barrier coatings: A review and current status7. Unleashing the Potential of Ceramic Matrix Composites for Hypersonic Flight8. ZrO2 reinforced ablative material suitable for the thermal protection system of ultra-high temperature in solid rocket motor combustion chamber9. 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