session 4

Title: Advanced Materials and Structures for High Temperature Applications
type: oral
Description: The topics to be addressed include advanced materials and structures for high temperature applications in space related domains. This includes carbon-carbon and ceramic matrix composites, ultra high temperature ceramics, ablative materials, ceramic tiles and insulations, together with innovative structural concepts making use of the above, for propulsion systems, launchers, hypersonic vehicles, entry vehicles, aero capture, power generation. The session covers the full spectrum of material, design, manufacturing and testing aspects.
Date: 2022-09-20
Time: 10:15
Room: W06

IPC members

Co-Chair: Dr. David E. Glass, National Aeronautics and Space Administration (NASA), United States;
Co-Chair: Mr. Thierry Pichon, ArianeGroup, France;
Rapporteur: Dr. Zijun Hu, China Academy of Launch Vehicle Technology (CALT), China;

papers
Order	Time	Paper title	Mode	Presentation status	Speaker	Affiliation	Country
1	10:15	KEYNOTE: Paolo Santini's Memorial Lecture - Active damping, vibration isolation and shape control of space structures	30	confirmed	Prof. André Preumont	University of Brussels	Belgium
2	10:45	a novel thermal protection system via opposing jet arrays for reusable reentry vehicles	11	confirmed	Dr. Xiaoyan Li	CASC	China
3	10:56	In-situ emissivity assessment of grade 5 titanium in high-enthalpy flows for catalysis investigations	11	confirmed	Mr. Clemens Felix Kaiser	University of Stuttgart	Germany
4	11:07	Innovative superalloy powder designed for Additive Manufacturing and for high temperature use up to 900°C	11	confirmed	Mrs. Solange Vivès	Aubert & Duval	France
5	11:18	Preliminary design of the heat shield for a Mars entry vehicle	11	withdrawn	Mr. Gianmarco Floro	Politecnico di Torino	Italy
6	11:29	Thermo structural analysis and test results of solid rocket motor submerged Nozzle throat with 4-D Carbon-Carbon (C-C) and graphite material	11	confirmed	Mr. Paul Murugan J	Vikram Sarabhai Space Centre, ISRO, Thiruvananthapuram	India
7	11:40	performance enhancement of cooler micro-vibration isolation system by implementing thermal design with graphite sheet	11	confirmed	Ms. Hye-In Kim	Chosun University	Korea, Republic of
8	11:51	Design of thermal protection based on carbon aerogel composite with optimal structure	11	confirmed	Ms. Margarita Salosina	Moscow Aviation Institute (National Research University)	Russian Federation
9	12:02	Development of the analysis methods for Solar probe thermal protection	11	confirmed	Dr. Alena V. Morzhukhina	Moscow Aviation Institute (National Research University, MAI)	Russian Federation
10	12:13	Anisotropic Heat-Shielding Materials based on Glass Carbon and Pyrolytic Graphite: Evaluation of Effectiveness in case of a Re-entry Module of a Lunar Probe	11	confirmed	Dr. Victor Leonov	Bauman Moscow State Technical University	Russian Federation
11	12:24	Improvements in PI Aerogels for Flexible Thermal Protection System - Hypersonic Inflatable Aerodynamic Decelerator (HIAD)	11	confirmed	Mr. Tushar Agarwal	Sardar Vallabhbhai National Institute of Technology Surat	India
12	12:35	Space Rider: Thermal Protection System and Control Surfaces design, development and qualification status	11	confirmed	Dr. Giuseppe Rufolo	CIRA Italian Aerospace Research Centre	Italy

session 4

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