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

    Papers

    1. KEYNOTE: Paolo Santini's Memorial Lecture: Ablators from Apollo to Future Missions to Moon, Mars, and Beyond

    2. Designing Building and Testing of a Thermal Protection System for a Spacecraft Which Cannot be Qualified Using the Standard Methodology

    3. Parker Solar Probe Structural-Thermal Analysis Challenges

    4. Effect of SiC concentration on aero-thermal behavior of ZrB2-based ceramics in hypersonic environment

    5. Design and experimental analysis of a three-segment sandwich structure nose cone for hypersonic vehicle with a compare study of numerical simulation experimental method

    6. Design and experimental verification research of a convenient high temperature resistance self-lubricating CMC hinge for control surface of hypersonic vehicle

    7. Structural Design and Analysis of an Aeroshell for a Human crew Re-entry Vehicle

    8. Protective heat resistant coating for Inconel 718 additively manufactured parts

    9. Extreme-Temperature Carbon- and Ceramic-Matrix Composite Nozzle Extensions for Liquid Rocket Engines

    10. C/C-SiC CERAMIC MATRIX COMPOSITE ORBITAL THRUSTER DEVELOPMENT FOR HPGP OPERATION

    11. Method of heat-proof nickel alloys mechanical properties improvement for rocket engines

    12. An active and passive combined thermal protection technology for flow distribution in parallel channels

    . Morphology and Anti-ablation Properties of Composites Nozzles under the Ф100mm H2O2- PE Hybrid Rocket Motor Test