Thermal performance and ablation characteristics of C/C-SiC for thermal protection of hypersonic vehicle
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Title
Thermal performance and ablation characteristics of C/C-SiC for thermal protection of hypersonic vehicle
Authors
Keywords
C/C-SiC composite material, Ablation rates, Ablation characteristics, Thermal protection performance
Journal
JOURNAL OF THE EUROPEAN CERAMIC SOCIETY
Volume -, Issue -, Pages -
Publisher
Elsevier BV
Online
2021-03-18
DOI
10.1016/j.jeurceramsoc.2021.03.015
References
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Note: Only part of the references are listed.- Effects of Oxygen Content on the Ablation Behavior of Silicone Rubber-Based Insulation Material
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- (2012) Si’an Chen et al. CORROSION SCIENCE
- Experimental investigation of passive/active oxidation behavior of SiC based ceramic thermal protection materials exposed to high enthalpy plasma
- (2012) Isil Sakraker et al. JOURNAL OF THE EUROPEAN CERAMIC SOCIETY
- Oxidation behavior of oxidation protective coatings for PIP–C/SiC composites at 1500°C
- (2011) Yang Xiang et al. CERAMICS INTERNATIONAL
- Morphology and microstructure of 2.5 dimension C/SiC composites ablated by oxyacetylene torch
- (2008) Dan Fang et al. CERAMICS INTERNATIONAL
- Silica on Silicon Carbide
- (2008) Volker Presser et al. CRITICAL REVIEWS IN SOLID STATE AND MATERIALS SCIENCES
- HfB2/SiC as a protective coating for 2D Cf/SiC composites: Effect of high temperature oxidation on mechanical properties
- (2007) M. Pavese et al. SURFACE & COATINGS TECHNOLOGY
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