Material property requirements for analysis and design of UHTC components in hypersonic applications
- 1 August 2010
- journal article
- Published by Elsevier BV in Journal of the European Ceramic Society
- Vol. 30 (11), 2239-2251
- https://doi.org/10.1016/j.jeurceramsoc.2010.01.026
Abstract
No abstract availableThis publication has 43 references indexed in Scilit:
- Thermal and Electric Properties in Hot‐Pressed ZrB2–MoSi2–SiC CompositesJournal of the American Ceramic Society, 2007
- Refractory Diborides of Zirconium and HafniumJournal of the American Ceramic Society, 2007
- Resistance to Thermal Shock and to Oxidation of Metal Diborides–SiC Ceramics for Aerospace ApplicationJournal of the American Ceramic Society, 2007
- Long-term oxidation behavior and mechanical strength degradation of a pressurelessly sintered ZrB2–MoSi2 ceramicScripta Materialia, 2005
- Oxidation behavior of a pressureless sintered ZrB2–MoSi2 ceramic compositeJournal of Materials Research, 2005
- Processing, properties and arc jet oxidation of hafnium diboride/silicon carbide ultra high temperature ceramicsJournal of Materials Science, 2004
- Oxidation-based materials selection for 2000°C + hypersonic aerosurfaces: Theoretical considerations and historical experienceJournal of Materials Science, 2004
- High‐Strength Zirconium Diboride‐Based CeramicsJournal of the American Ceramic Society, 2004
- Oxidation of ZrB[sub 2]-Based Ceramics in Dry AirJournal of the Electrochemical Society, 2003
- Mechanical, Thermal, and Oxidation Properties of Refractory Hafnium and zirconium CompoundsJournal of the European Ceramic Society, 1999