Oxidation of ZrB2-SiC: Comparison of furnace heated coupons and self-heated ribbon specimens

Ceramic Engineering and Science Proceedings

Volumn 28, Issue 2, 2008, Pages 327-336

  Karlsdottir, S N ^a   Halloran, J W ^a   Monteverde, F ^b   Bellosi, A ^b  

^a UNIVERSITY OF MICHIGAN   (United States)

^b INSTITUTE OF SCIENCE AND TECHNOLOGY FOR CERAMICS   (Italy)

Author keywords

[No Author keywords available]

Indexed keywords

AMBIENT AIRS; CONVENTIONAL FURNACES; CYCLIC OXIDATIONS; OXIDE SCALES; SURFACE LAYERS; TWO DIFFERENT METHODS;

CARBON FIBER REINFORCED PLASTICS; CERAMIC MATERIALS; FURNACES; MECHANICAL PROPERTIES; OXIDATION; SCALE (DEPOSITS); SILICON COMPOUNDS; ZIRCONIUM ALLOYS;

SILICON CARBIDE;

EID: 57649166999     PISSN: 01966219     EISSN: None     Source Type: Conference Proceeding    
DOI: None     Document Type: Conference Paper

References (22)

1. M. M. Opeka, I.G. Talmy, and J.A. Zaykoski, "Oxidation-Based Materials Selection for 2000°C + Hypersonic Aerosurface: Theoretical Considerations and Historical Experience," J. of Mater. Sci., 39 [19] 5887-5904 (2004).
2. P. Kolodziej, "Aerothermal Performance Constraints for Hypervelocity Small Radius Unswept Leading Edges and Nosetips," NASA Technical Memorandum 112204, July (1997).
3. R. Reidel, Handbook of Ceramic Hird Materials, vol. 2, chapter: Transition Metal Boride Ceramics, pp. 881, Wiley-VCH, Weinheim, Germany (2000).
4. C. Mroz, "Annual Mineral Review: Zirconium Diboride," Am. Ceram. Soc. Bull. 74 [6] 165-166 (1995)
5. L. Kaufman, "Boride Composites - A New Generation of Nose Cap and Leading Edge Materials for Reusable Lifting Reentry Systems," AIAA Advanced Space Transportation Meeting. American Institute of Aeronautics and Astronautics, AIAA 270-278 (1970).
6. L. Kaufman and H. Nesor, "Stability Characterization of Refractory Materials under High Velocity Atmospheric Flight Conditions. Part I, Vol. I, Summary," Technical Report no. AMFL-TR-69-84, Air Force Materials Laboratory, Wright-Patterson Air Base, OH (1970).
7. C A. Hoffman, "Preliminary Investigation of Zirconium Boride Caramels for GasTurbine Blade Applicatons," NASA Technical Memorandum E52L15a, Lewis Flight Propulsion Laboratory, Cleveland, OH (1953).
8. 2 in Temperature Range of 800 Degrees to 1500 Degrees." Journal of the Electrochemical Society, 118 [7] 1195-1971 (1971).
9. 2," Am. Ceram. Soc. Bull., 52 [8] 612-616 (1973).
10. F. Monteverde, A. Bellosi and S. Guicciardi, "Processing and Properties of Zirconium Diboride-Based Composites," J. Eur. Ceram. Soc., 22 279-288 (2002).
11. 2-Based Ceramics in Dry Air," Journal of the Electrochemical Society, 150 [11] B-552-B559 (2003).
12. F. Monteverde and A. Bellosi. "Development and Characterization of Metal-Diboride-Based Composites Toughened with Ultra-Fine SiC Particulates," Solid State Sciences, 7 [5] 622-630 (2005).
13. 2-SiC Ceramics under Atmospheric and Reentry Conditions," Refractories Applications Transactions, 1 [2] 1-8 (2005).
14. M. M. Opeka, I.G. Talmy, E.J. Wuchina, J.A. Zaykoski and S.J. Causey. "Mechanical, Thermal, and Oxidation Properties of Refractory Hafnium and Zirconium Compounds," J. Eur. Ceram. Soc., 19 2405-2414 (1999).
15. S. R. Levine, E.J. Opila, M. C. Halbig, J. D. Kiser, M. Singh and J. A. Salem. "Evaluation of Ultra-High Temperature Ceramics for Aeropropulsion Use," J. Eur. Ceram. Soc., 22 2757-2767 (2002).
16. 2 based Ultra-High Temperature Ceramics: Effect of Ta Additions," Journal of Materials Science, 39 5969-5977 (2004).
17. S. N. Karlsdottir, and J.W. Halloran. (Accepted to the J. Am. Ceram. Soc., April 2007).
18. 2-SiC Composite." J. Eur. Ceram. Soc. 25 1025-1031 (2005).
19. M. Gasch, D. Ellerby, E. Irby, S. Beckman, M. Gusman, & S. Johnson. "Processing, Properties and Arc Jet Oxidation of Hafnium Diboride/Silicon Carbide Ultra High Temperature Ceramics." Journal of Materials Science 39 5925-5937 (2004).
20. 2-SiC Oxidation: Formation of a SiC-Depleted Region." J. Am. Ceram. Soc., 90 [1] 143-148 (2007).
21. 2" Appl. Phys. A 82 329-337 (2006)
22. A. Rezaie, W.G. Fahrenholtz, and G.E. Hilmas, "Evolution of Structure during the Oxidation of Zirconium Diboride-Silicon Carbide in Air up to 1500C," J. Eur. Ceram. Soc. 27 [6] 2495-2501 (2007).