rootbrowseIAC-19C2session 44. Advanced Materials and Structures for High Temperature ApplicationsPapers1. KEYNOTE: Paolo Santini's Memorial Lecture: Ablators from Apollo to Future Missions to Moon, Mars, and Beyond2. Designing Building and Testing of a Thermal Protection System for a Spacecraft Which Cannot be Qualified Using the Standard Methodology3. Parker Solar Probe Structural-Thermal Analysis Challenges4. Effect of SiC concentration on aero-thermal behavior of ZrB2-based ceramics in hypersonic environment5. Design and experimental analysis of a three-segment sandwich structure nose cone for hypersonic vehicle with a compare study of numerical simulation experimental method6. Design and experimental verification research of a convenient high temperature resistance self-lubricating CMC hinge for control surface of hypersonic vehicle7. Structural Design and Analysis of an Aeroshell for a Human crew Re-entry Vehicle8. Protective heat resistant coating for Inconel 718 additively manufactured parts9. Extreme-Temperature Carbon- and Ceramic-Matrix Composite Nozzle Extensions for Liquid Rocket Engines10. C/C-SiC CERAMIC MATRIX COMPOSITE ORBITAL THRUSTER DEVELOPMENT FOR HPGP OPERATION11. Method of heat-proof nickel alloys mechanical properties improvement for rocket engines12. 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