Multilayer SiC for thermal protection system of space vehicles with decreased thermal conductivity through the thickness

Author:

Biamino S.,Antonini A.,Eisenmenger-Sittner C.,Fuso L.,Pavese M.,Fino P.,Bauer E.,Badini C.

Publisher

Elsevier BV

Subject

Materials Chemistry,Ceramics and Composites

Reference44 articles.

1. Technologies for thermal protection systems applied on re-usable launcher;Behrens;Acta Astronaut,2004

2. A collection of technical papers. 13th AIAA/CIRA international space planes and hypersonic systems and technologies conference;Scatteia,2005

3. Oxidation-resistant ZrB2–SiC composites at 2200°C;Han;Comp Sci Technol,2008

4. Evaluation of ultra-high temperature ceramics for aeropropulsion use;Levine;J Eur Ceram Soc,2002

5. Aerothermodynamic study of UHTC-based thermal protection systems;Savino;Aerospace Sci Technol,2005

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