Emissivity and catalycity measurements on SiC-coated carbon fibre reinforced silicon carbide composite

Journal of the European Ceramic Society

Volumn 29, Issue 10, 2009, Pages 2045-2051

  Alfano, Davide ^a   Scatteia, Luigi ^a   Cantoni, Stefania ^a   Balat Pichelin, Marianne ^b  

^a ITALIAN AEROSPACE RESEARCH CENTER   (Italy)

^b Centre National de la Recherche Scientifique   (France)

Author keywords

B. Composites; C. Chemical properties; C. Optical properties; D. Carbon SiC; Thermal protection system

Indexed keywords

B. COMPOSITES; C. CHEMICAL PROPERTIES; C. OPTICAL PROPERTIES; D. CARBON/SIC; THERMAL PROTECTION SYSTEM;

CARBON FIBERS; CARBON NANOFIBERS; ELECTROMAGNETIC WAVE EMISSION; HEAT SHIELDING; OPTICAL PROPERTIES; OXYGEN; SILICA; THERMAL INSULATING MATERIALS;

SILICON CARBIDE;

EID: 67349110436     PISSN: 09552219     EISSN: None     Source Type: Journal    
DOI: 10.1016/j.jeurceramsoc.2008.12.011     Document Type: Article

References (53)

1. Naslain R. High Temperature Ceramic Matrix Composites (1993), Woodhead Publications, Bordeaux pp. 215-229
2. Laux T., Ullmann T., Auweter-Kurtz M., Hald H., and Kurz A. Investigation of thermal protection materials along an X-38 re-entry trajectory by plasma wind tunnel simulations. Proceeding of the 2nd International Symposium on Atmospheric Reentry Vehicles and Systems. Arcahon (2001) 1-9
3. Naslain R., Lamalle J., and Zulian J.L. Composite materials for high temperature applications. Proceedings of the AMAC. Paris (1990) 315-325
4. Messiah A. Developments in the Science and Technology of Composite Materials (1989), Elsevier, London pp. 99-110
5. Chawla N., Holmes J.W., and Lowden R.A. The role of interfacial coatings on the high frequency fatigue behavior of Nicalon/C/SiC composites. Scr. Mater. 35 (1996) 1411-1416
6. Lamouroux F., Bourrat X., Sevely J., and Naslain R. Structure/oxidation behaviour relationship in the carbonaceous constituents of 2D-C/PyC/SiC composites. Carbon 31 (1993) 1273-1288
7. Torben K.J., and Povl B. Mechanical properties of two plain-woven chemical vapor infiltrated silicon carbide-matrix composites. J. Am. Ceram. Soc. 84 (2001) 1043-1051
8. Mühlratzer A., and Leuchs M. Applications of non-oxide CMCs. Proceedings of the 4th International Conference on High Temperature Ceramic Matrix Composites. Munich, Germany, October 1-3 (2001) 288-298
9. Harnisch B., Kunkel B., Deyerler M., Bauereisen S., and Papenburg U. Ultra-lightweight C/SiC mirrors and structures. ESA Bull. 95 (1998) 4-8
10. Heuer A.H., and Lou V.L.K. Volatility diagrams for silica, silicon nitride, and silicon carbide and their application to high temperature decomposition and oxidation. J. Am. Ceram. Soc. 73 (1990) 2785-3128
11. Schneider B., Guette A., Naslain R., Cataldi M., and Costecalde A. A theoretical and experimental approach to the active-to-passive transition in the oxidation of silicon carbide. J. Mater. Sci. 33 (1998) 535-547
12. Jacobson N.S. Corrosion of silicon-based ceramics in combustion environments. J. Am. Ceram. Soc. 76 (1993) 3-28
13. 2-SiC oxidation: formation of a SiC-depleted region. J. Am. Ceram. Soc. 90 (2006) 143-148
14. Balat M.J.H. Determination of the active-to-passive transition in the oxidation of silicon carbide in standard and microwave-excited air. J. Eur. Ceram. Soc. 16 (1996) 55-62
15. Morino Y., Yoshinaka T., Auweter-Kurtz M., Hilfer G., Speckmann H.-D., and Sakai A. Erosion characteristics of SiC coated C/C materials in arc heated high enthalpy air flow. Acta Astro. 50 (2002) 149-158
16. Opeka M.M., Talmy I.G., and Zaykoski J.A. Oxidation-based materials selection for 2000 °C + hypersonic aerosurfaces: theoretical considerations and historical experience. J. Mater. Sci. 39 (2004) 5887-5904
17. Rezaie A., Fahrenholtz W.G., and Hilmas G.E. Evolution of structure during the oxidation of zirconium diboride-silicon carbide in air up to 1500 °C. J. Eur. Ceram. Soc. 27 (2007) 2495-2501
18. Damjanović T., Argirusis C., Jokanovíc B., Borchardt G., Moritz K., Müller E., et al. Oxidation protection of C/C-SiC composites by an electrophoretically deposited mullite precursor: cyclic thermogravimetric analysis. J. Eur. Ceram. Soc. 27 (2007) 1299-1302
19. Cheng L., Xu Y., Zhang L., and Yin X. Effect of coating defects on oxidation behaviour of three dimensional C/SiC composites from room temperature to 1500 °C. J. Mater. Sci. 37 (2002) 5339-5344
20. 2 oxidation protection coating. J. Mater. Sci. 34 (1999) 6009-6014
21. Piquero T., Vincent H., Vincent C., and Bouix J. Influence of carbide coatings on the oxidation behaviour of carbon fibers. Carbon 33 (1995) 455-467
22. Webster J.D., Westwood M.E., Hayes F.H., Day R.J., Taylor R., Duran A., et al. Oxidation protection coatings for C/SiC based on yttrium silicate. J. Eur. Ceram. Soc. 18 (1998) 2345-2350
23. Zhang Y.-L., Li H.-J., Fu Q.-G., Li K.Z., Hou D.-S., and Fei J. A Si-Mo oxidation protective coating for C/SiC coated carbon/carbon composites. Carbon 45 (2007) 1105-1136
24. Zhang Y.-L., Li H.-J., Fu Q.-G., Li K.Z., Wei J., and Wang P.-Y. A C/SiC gradient oxidation protective coating for carbon/carbon composites. Surf. Coat. Technol. 201 (2006) 3491-3495
25. Van Wie D.M., Drewry Jr. D.G., King D.E., and Hudson C.M. The hypersonic environment: required operating conditions and design challenges. J. Mater. Sci. 39 (2004) 5915-5924
26. Henline W.D. Thermal protection analysis of Mars-Earth return vehicles. J. Spacecraft Rockets 29 (1992) 198-207
27. Williams S.D., Curry D.M., Bouslog S.A., and Rochelle W.C. Thermal protection system design studies for lunar crew module. J. Spacecraft Rockets 32 (1995) 198-207
28. Steinacher A., Lange H., Weiland S., and Hudrisier S. Development of CMC body flaps for future re-entry vehicles. Proceedings of the 58th International Astronautical Congress. Hyderabad, India, September 24-28 (2007)
29. Hald H., and Winkelmann P. TPS development by ground and reentry flight testing of CMC materials and structures. Proceedings of 2nd European Workshop on Thermal Protection Systems (ESA). Stuttgart, Germany, October 23-27 (1995)
30. Hald H., and Winkelmann P. Post mission analysis of the heat shield experiment CETEX for the EXPRESS capsule. Proceedings of the 48th International Astronautical Congress. International Astronautical Federation. Turin, Italy, October 6-10 (1997)
31. Brix P., and Herzberg G. The dissociation energy of oxygen. J. Chem. Phys. 21 (1953) 2240
32. 2. Phys. Rev. 96 (1954) 1540-1542
33. Scott C.D. Catalytic recombination of oxygen and nitrogen in high temperature reusable surface insulation. In: Crosbie A.L. (Ed). Progress in Astronautics and Aeronautics: Aerothermodynamics and Planetary Entry (1981), AIAA, New York 192-212
34. Rakich, J. V., Stewart, D. A. and Lanfranco, M. J., Results of a flight experiment on the catalytic efficiency of the Space Shuttle heat shield. AIAA Paper 82-0944, June 1982.
35. Stewart, D. A., Rakich, J. V. and Lanfranco, M. J., Catalytic surface effects on space shuttle thermal protection system during earth entry of flights STS-2 through STS-5. NASA CP-2283, Part 2, 1983, p. 827.
36. Scott C.D. Effects of nonequilibrium and wall catalysis on shuttle heat transfer. J. Spacecraft Rockets 41 (1985) 489-499
37. 2/SiC ultrahigh-temperature ceramic composites. J. Spacecraft Rockets 41 (2004) 576-581
38. Dogigli M., Pradier A., and Tumino G. Advanced key technologies for hot control surfaces in space re-entry vehicles. Proceedings of the 34th COSPAR Scientific Assembly. Huston, TX, October 10-19 (2002)
39. Dogigli M., Pfeiffer H., Eckert A., and Fröhlich A. Qualification of CMC body flaps for X-38. Proceedings of the 52nd International Aeronautical Congress. Toulouse, France, October 1-5 (2001)
40. Mühlratzer A., Köberle H., Peetz K., and Wildenrotter K. Design and manufacture of CMC materials for reentry vehicles. Proceedings of the 3rd European Workshop on TPS. Noordwijk, Netherlands, November 24-26 (1998)
41. Balat-Pichelin M., Robert J.F., and Sans J.L. Emissivity measurements on carbon-carbon composites at high temperature under high vacuum. Appl. Surf. Sci. 253 (2006) 778-783
42. Balat-Pichelin M., Hernandez D., Olalde G., Rivoire B., and Robert J.F. Concentrated solar energy as a diagnostic tool to study materials under extreme conditions. J. Sol. Energy Trans. ASME 124 (2002) 215-222
43. Paulmier T., Balat-Pichelin M., Le Quéau D., Berjoan R., and Robert J.F. Physico-chemical behaviour of carbon materials under high temperature and ion irradiation. Appl. Surf. Sci. 180 (2001) 227-245
44. Paulmier T., Balat-Pichelin M., and Le Quéau D. Structural modifications of carbon-carbon composites under high temperature and ion irradiation. Appl. Surf. Sci. 243 (2005) 376-393
45. Dunlap Jr. P.H., Steinetz B.M., Curry D.M., and DeMange J.J. Investigations of a control surface seal for reentry vehicle. J. Spacecraft Rockets 40 (2003) 570-583
46. Cleland, J. and Iannetti, F., Thermal protection system of the space shuttle. NASA CR-4227, N89-26046, 1989.
47. Balat-Pichelin M., Badie J.M., Berjoan R., and Boubert P. Recombination coefficient of atomic oxygen on ceramic materials under earth re-entry conditions by optical emission spectroscopy. Chem. Phys. 291 (2003) 181-194
48. 3 at high temperature under air microwave-induced plasma. Chem. Phys. 340 (2007) 217-226
49. Balat M., Czerniak M., and Badie J.M. Thermal and chemical approaches for oxygen catalytic recombination evaluation on ceramic materials at high temperature. Appl. Surf. Sci. 120 (1997) 225-238
50. Balat-Pichelin M., and Vesel A. Neutral oxygen atom density in the MESOX air plasma solar furnace facility. Chem. Phys. 327 (2006) 112-118
51. 2-SiC ultrahigh temperature ceramic composites. J. Spacecraft Rockets 43 (2006) 1004-1012
52. 2-based ceramics. J. Am. Ceram. Soc. 91 (2008) 1461-1468
53. Arrhenius S. Uber die Reaktionsgeschwindigkeit bei der Inversion von Rohrzucker durch Sauren. Z. Phys. Chem. 4 (1889) 226