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

    Papers

    1. obtention of a carbon-carbon composite material for its use in expanding nozzles for aerospace vehicles.

    3. Development and flight test of a suborbital re-entry demonstrator

    6. Anisotropic Heat-Shielding Materials: Evaluation of Effectiveness in case of a Re-entry Module

    7. Advanced Materials for Thermal Management of Superconductor-Based Spacecraft Systems

    8. Experimental and numerical studies of MHD effects on plasma flows for re-entry applications

    9. The Implementation of the Alginate Montmorillonite Nanocomposite Foam into Heat Shields

    10. Thermal Fatigue Analysis of FGM Base Plate of Satellite Structures

    1012. Estimation of EPDM insulation ablation considering variable properties