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  • session 4
  • 4. Advanced Materials and Structures for High Temperature Applications

    Papers

    1. irene technology for Thermal protection systems

    2. hexafly-int hypersonic vehicle thermal protection system design

    4. Structural Design and Analysis of an Aeroshell for a Human Crew Entry Vehicle in Martian Atmosphere

    6. Aero-thermo-dynamic Characterization of Large-scale Near-zero Ablation Thermal Protection Systems in Ultra-High-Temperature Ceramic Matrix Composites

    7. Interaction of BN-coated carbon fibres with TiC-based ultra-high temperature ceramics matrices in oxidizing environments around 2500 °C

    8. Architected Ceramic Structures for High Temperature Applications

    9. Thermal History Coatings for Thermal Protection Systems

    10. Thermo structural assessment of upper stage solid rocket motor Nozzle throat with 4-D Carbon Carbon (C-C) and graphite material

    11. OBTENTION OF A CARBON-CARBON COMPOSITE MATERIAL FOR ITS USE IN EXPANDING NOZZLES FOR AEROSPACE VEHICLES.

    12. MORPHOLOGY AND ANTI-ABLATION PROPERTIES OF COMPOSITES NOZZLES UNDER THE Ф100MM H2O2- PE HYBRID ROCKET MOTOR TEST