Thermal Performance of Ablative/ Ceramic Composite
A hybrid thermal protection system for atmospheric earth re-entry based on ablative materials on top of ceramic matrix composites is investigated for the protection of the metallic structure in oxidative and high temperature environment of the space vehicles. The paper focuses on the joints of ablat...
Main Authors: | , , , , , , , , , , , , , , |
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Format: | Article |
Language: | English |
Published: |
National Institute for Aerospace Research “Elie Carafoli” - INCAS
2014-12-01
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Series: | INCAS Bulletin |
Subjects: | |
Online Access: | http://bulletin.incas.ro/files/stefan__colab_vol_6_iss_4.pdf |