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: 2019-10-23
Time: 09:45
Room: 152B

IPC members

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

papers
Order	Time	Paper title	Mode	Presentation status	Speaker	Affiliation	Country
1	09:45	KEYNOTE: Paolo Santini's Memorial Lecture: Ablators from Apollo to Future Missions to Moon, Mars, and Beyond	24	confirmed	Dr. Ethiraj Venkatapathy	NASA Ames Research Center	United States
2	10:09	Designing Building and Testing of a Thermal Protection System for a Spacecraft Which Cannot be Qualified Using the Standard Methodology	12	confirmed	Mr. edward schaefer	JHU Applied Physics Laboratory	United States
3	10:21	Parker Solar Probe Structural-Thermal Analysis Challenges	12	confirmed	Mrs. Shelly Conkey	JHU Applied Physics Laboratory	United States
4	10:33	Effect of SiC concentration on aero-thermal behavior of ZrB2-based ceramics in hypersonic environment	12	confirmed	Mr. Stefano Mungiguerra	Università degli Studi di Napoli “Federico II”	Italy
5	10:45	Design and experimental analysis of a three-segment sandwich structure nose cone for hypersonic vehicle with a compare study of numerical simulation experimental method	18	withdrawn	Mr. XIANG ZHANG	China Academy of Launch Vehicle Technology(CALT)	China
6	11:03	Design and experimental verification research of a convenient high temperature resistance self-lubricating CMC hinge for control surface of hypersonic vehicle	18	withdrawn	Mr. XIANG ZHANG	China Academy of Launch Vehicle Technology(CALT)	China
7	11:21	Structural Design and Analysis of an Aeroshell for a Human crew Re-entry Vehicle	12	no-show	Mr. Shaun Andrews	University of Bristol	United Kingdom
8	11:33	Protective heat resistant coating for Inconel 718 additively manufactured parts	12	confirmed	Mr. Nickolay (Mykola) Gorulya (Horulia)	Firefly Aerospace Inc.	Ukraine
9	11:45	Extreme-Temperature Carbon- and Ceramic-Matrix Composite Nozzle Extensions for Liquid Rocket Engines	12	confirmed	Mr. Peter Valentine	National Aeronautics and Space Administration (NASA)	United States
10	11:57	C/C-SiC CERAMIC MATRIX COMPOSITE ORBITAL THRUSTER DEVELOPMENT FOR HPGP OPERATION	12	no-show	Mr. Ilja Mueller	German Aerospace Center (DLR)	Germany
11	12:09	Method of heat-proof nickel alloys mechanical properties improvement for rocket engines	12	confirmed	Ms. Maryna Hrekova	Yuzhnoye State Design Office	Ukraine
12	12:21	An active and passive combined thermal protection technology for flow distribution in parallel channels	12	confirmed	Mr. Chen Siyuan	China Academy of Aerospace Aerodynamics (CAAA)	China
*		Identifying non-linear heat transfer states of a spacecraft’s heat shield during its entry into the atmosphere by using the comparative test method		confirmed	Mr. Yang Tianyang	Moscow Aviation Institute (National Research University, MAI)	Russian Federation

session 4

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