Ablation tests on HfC- and TaC-based ceramics for aeropropulsive applications-Reference-Cited by-同舟云学术

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Ablation tests on HfC- and TaC-based ceramics for aeropropulsive applications

Published:2015-05 Issue:5 Volume:35 Page:1401-1411
ISSN:0955-2219
Container-title:Journal of the European Ceramic Society
language:en
Short-container-title:Journal of the European Ceramic Society

Author:

Pienti L.,Sciti D.^ORCID,Silvestroni L.,Cecere A.,Savino R.

Publisher

Elsevier BV

Subject

Materials Chemistry,Ceramics and Composites

Reference28 articles.

1. Ultra high temperature assessment study: ceramic matrix composites;Courtright,1992

2. Performances of rocket nozzle material with several solid propellants;Johnston,1966

3. Net shape fabrication of high temperature materials for rocket engine components;Hickman,2011

4. Oxidation resistant HfC–TaC rocket thruster for high performance propellants, NAS3-27272;Patterson,1999

5. The refractories HfC and HfN – a survey I and II;Perry;Powder Metall Int,1987

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