Determination of heat capacity of carbon composites with application to carbon/phenolic ablators up to high temperatures-Reference-Cited by-同舟云学术

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Determination of heat capacity of carbon composites with application to carbon/phenolic ablators up to high temperatures

Published:2021-01 Issue: Volume:108 Page:106375
ISSN:1270-9638
Container-title:Aerospace Science and Technology
language:en
Short-container-title:Aerospace Science and Technology

Author:

Torres-Herrador Francisco^ORCID,Turchi Alessandro,Van Geem Kevin M.^ORCID,Blondeau Julien,Magin Thierry E.

Funder

Research Foundation Flanders

European Space Agency

Horizon 2020

Publisher

Elsevier BV

Subject

Aerospace Engineering

Reference41 articles.

1. Ablative Thermal Protection Systems Modeling;Duffa,2013

2. Space Debris: Models and Risk Analysis;Klinkrad,2006

3. A comparison of commonly used re-entry analysis tools;Lips;Acta Astronaut.,2005

4. A Short Review of Ablative-Material Response Models and Simulation Tools;Lachaud,2011

5. Post-flight evaluation of stardust sample return capsule forebody heatshield material;Stackpoole,2008

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1. Stochastic mesoscale characterization of ablative materials for atmospheric entry;Applied Mathematical Modelling;2024-11

2. Intricacies of high temperature thermal characterization of Silicaf/Silica composites;Journal of the European Ceramic Society;2024-09

3. Effects of pyrolysis reaction and gas characteristics on the thermal response of resin-based ablative materials;Applied Thermal Engineering;2024-09

4. Experimental Study of Thermomechanical Characteristics of C/ARMC Composites at High Temperatures as Thermal Protection Systems for Aerospace Applications;Journal of The Institution of Engineers (India): Series C;2024-07-20

5. Ablation simulation of integral woven gradient three‐dimensional thermal protection structures for planetary exploration;Polymer Composites;2024-07-12

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