Thermal Conductivity Evolution of Carbon-Fiber Ablators Submitted to High Temperatures-Reference-Cited by-同舟云学术

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Thermal Conductivity Evolution of Carbon-Fiber Ablators Submitted to High Temperatures

Published:2022-10 Issue:4 Volume:36 Page:940-950
ISSN:1533-6808
Container-title:Journal of Thermophysics and Heat Transfer
language:en
Short-container-title:Journal of Thermophysics and Heat Transfer

Author:

Turchi Alessandro¹^ORCID,Torres-Herrador Francisco¹^ORCID,Helber Bernd¹,Pintsuk Gerald²,Zuber Christian³,Ritter Heiko⁴,Magin Thierry E.¹

Affiliation:

1. von Karman Institute for Fluid Dynamics, 1640 Rhode-Saint-Genèse, Belgium

2. Forschungszentrum Jülich, GmbH, 52425 Jülich, Germany

3. DLR, German Aerospace Center, 70569 Stuttgart, Germany

4. European Space Agency, 2200 AG Noordwijk, The Netherlands

Funder

European Space Agency

Publisher

American Institute of Aeronautics and Astronautics (AIAA)

Subject

Condensed Matter Physics,Aerospace Engineering,Space and Planetary Science,Fluid Flow and Transfer Processes,Mechanical Engineering

Link

https://arc.aiaa.org/doi/pdf/10.2514/1.T6485

Reference26 articles.

1. Performance of a Low Density Ablative Heat Shield Material

2. Experimental investigation of ablation and pyrolysis processes of carbon-phenolic ablators in atmospheric entry plasmas

3. Erratum on "Performance of a Low Density Ablative Heat Shield Material"

4. Erratum on "Erratum on 'Performance of a Low Density Ablative Heat Shield Material'"

5. Analysis of Galileo Probe Heatshield Ablation and Temperature Data

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2. Effect of the Internal Gas Flow Velocity on the Thermal Conductivity of Porous Thermal Protection Systems and Application to Stardust Re-Entry;AIAA SCITECH 2024 Forum;2024-01-04

3. High-temperature thermal conductivity measurements of macro-porous graphite;Proceeding of International Heat Transfer Conference 17;2023

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