session 4

Title

Advanced Materials and Structures for High Temperature Applications

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

2014-10-01

Time

09:45

Room

713A

IPC members
papers

Order

Time

Paper title

Selection result

Mode

Presentation status

Speaker

Affiliation

Country

1

Emissivity Analyses Of Materials Candidate For Eart’s Atmosphere Re-Entry From Space Missions

accepted

12'

confirmed

Dr. Carlo Purpura

CIRA Italian Aerospace Research Centre

Italy

2

estimation of surface heat flux for ablation and charring of thermal protection material

accepted

12'

no-show

Dr. Weiqi Qian

China Aerodynamics Research and Developement Center

China

3

Plasma Wind Tunnel Tests for C/SiC Composite with Additional Mechanical Tensile Load

accepted

12'

no-show

Mr. dongbin ou

China Academy of Aerospace Aerodynamics (CAAA)

China

4

Dynamic response testing and analysis of hypersonic aircraft panels excited by high-intensity acoustic loads in thermal environment

accepted

12'

no-show

Mr. Zhenqiang Wu

Beijing Institute of Structure and Environment Engineering

China

5

A new type scramjet thermal protection structure based on high temperature heat pipe technique

accepted

12'

confirmed

Prof.Dr. Ai Bangcheng

China Academy of Aerospace Aerodynamics (CAAA)

China

7

design study on multi-layered stand-off thermal protection system using porous titanium sandwich panels

accepted

12'

confirmed

Mr. Ryosuke Hayashi

Waseda University

Japan

8

A New Reusable Thermal Protection System Concept for Earth Atmospheric Re-Entry

accepted

12'

withdrawn

Dr. Jorge Barcena

Tecnalia Research and Innovation

Spain

9

Hybrid Ablative/Ceramic Thermal Protection System: Mission Profile, Materials Selection, Interface Development and Verification Approach

accepted

12'

withdrawn

Dr. Jorge Barcena

Tecnalia Research and Innovation

Spain

10

A Comparative Assessment of Criticality of Local Damage in Composite Liner of a Nozzle Through Finite Element Thermal-Structural Analysis

accepted

12'

confirmed

Mr. Thomas Kurian

Indian Space Research Organization (ISRO)

India

11

Thermally and Dimensionally Stable Structures of Carbon-Carbon Laminated Composites for Space Applications

accepted

12'

no-show

Dr. Volodymyr Slyvynskyi

“NIKE” Ltd. Scientific and Production Enterprise

Ukraine

12

The Ablative Performance of Light Weight Charring Ablators in High Enthalpy Environment

accepted

12'

no-show

Dr. HE GAO

China Academy of Aerospace Aerodynamics (CAAA)

China

13

Heat Pipe Cooled Leading Edges

accepted

12'

withdrawn

Dr. Suraj Rawal

Lockheed Martin Space Systems Company

United States