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

Journal of the European Ceramic Society

Volumn 30, Issue 8, 2010, Pages 1833-1840

  Biamino, S ^a   Antonini, A ^a   Eisenmenger Sittner, C ^b   Fuso, L ^c   Pavese, M ^a   Fino, P ^a   Bauer, E ^b   Badini, C ^a  

^a POLITECNICO DI TORINO   (Italy)

^b VIENNA UNIVERSITY OF TECHNOLOGY   (Austria)

^c Tecnogranda SPA   (Italy)

Author keywords

Mechanical properties; Multilayer; SiC; Tape casting; Thermal conductivity

Indexed keywords

CRACK DEFLECTIONS; DEBINDING; FRACTURE SURFACES; INSULATING COATINGS; LAYER STACKING; MULTI-LAYERED STRUCTURE; PARTIALLY STABILIZED ZIRCONIA; PORE-FORMING AGENTS; POROUS LAYERS; REDUCTION OF THERMAL CONDUCTIVITY; RESIDUAL POROSITY; ROOM TEMPERATURE; SIC; SPACE VEHICLES; TAPE CASTING; THERMAL PROTECTION SYSTEM;

BENDING STRENGTH; COATINGS; CRACKS; FRACTURE; HEAT SHIELDING; MULTILAYERS; SILICON CARBIDE; SINTERING; THERMAL CONDUCTIVITY; THERMAL INSULATING MATERIALS; THERMOANALYSIS; VEHICLES; YTTRIA STABILIZED ZIRCONIA; ZIRCONIA;

MECHANICAL PROPERTIES;

EID: 77950368147     PISSN: 09552219     EISSN: None     Source Type: Journal    
DOI: 10.1016/j.jeurceramsoc.2010.01.040     Document Type: Article

References (44)

1. Behrens B., Muller M. Technologies for thermal protection systems applied on re-usable launcher. Acta Astronaut 2004, 55:529-536.
2. Scatteia L., Borrelli R., Marino G., Bellosi A., Monteverde F. A collection of technical papers. 13th AIAA/CIRA international space planes and hypersonic systems and technologies conference 2005, 613. American Institute of Aeronautics and Astronautics.
3. 2-SiC composites at 2200°C. Comp Sci Technol 2008, 68:799-806.
4. Levine S.R., Opila E.J., Halbig M.C., Kiser J.D., Singh M., Salem J.A. Evaluation of ultra-high temperature ceramics for aeropropulsion use. J Eur Ceram Soc 2002, 22:2757-2767.
5. Savino R., De Stefano Fumo M., Paterna D., Serpico M. Aerothermodynamic study of UHTC-based thermal protection systems. Aerospace Sci Technol 2005, 9:151-160.
6. Monteverde F., Bellosi A., Scatteia L. Processing and properties of ultra-high temperature ceramics for space applications. Mater Sci Eng A 2008, 485:415-421.
7. Pichon T., Soyris P., Foucault A., Parenteau J.M., Prel Y., Guedron S. C/SiC based rigid external thermal protection system for future reusable launch vehicles: generic shingle, pre-X/FLPP anticipated development test studies. Proceedings of the 5th European workshop on " Thermal Protection Systems and Hot Structures" 2006, ESA-ESTEC, Noordwijk (The Netherlands).
8. Liedtke V., Huertas Olivares I., Langer M., Haruvy Y.F. Manufacturing and performance testing of sol/gel based oxidation protection systems for re-usable space vehicles. J Eur Ceram Soc 2007, 27:1493-1502.
9. Mue Hlratzer A., Handrick K., Pfeiffer H. Development of a new cost-effective ceramic composite for re-entry heat shield applications. Acta Astronaut 1998, 42/9:533-540.
10. Munro R.G. Material properties of a sintered α-SiC. J Phys Chem Ref Data 1997, 26(5):1195-1203.
11. Gulbransen E.A., Jansson S.A. The high-temperature oxidation, reduction, and volatilization reactions of silicon and silicon carbide. Oxid Metals 1972, 4(2):181-201.
12. Jacobson N.S., Fox D.S., Opila E.J. High temperature oxidation of ceramic matrix composites. Pure Appl Chem 1998, 70(2):493-500.
13. Clegg W.J. A simple way to make tough ceramics. Nature 1990, 347:455-457.
14. Clegg W.J. The fabrication and failure of laminar ceramic composites. Acta Metall Mater 1992, 40(11):3085-3093.
15. Vandeperre L., Van Der Biest O. Composite SiC-graphite interlayers for crack deflection in ceramic laminates. Silic Ind 1998, 63:39-43.
16. Blanks K.S., Kristoffersson A., Carlström E., Clegg W.J. Crack deflection in ceramic laminates using porous interlayers. J Eur Ceram Soc 1998, 18:1945-1951.
17. Davis J.B., Kristoffersson A., Carlström E., Clegg W.J. Fabrication and crack deflection in ceramic laminates with porous interlayers. J Am Ceram Soc 2000, 83:2369-2374.
18. Liu H., Hsu S.M. Fracture behaviour of multilayer silicon nitride/boron nitride ceramics. J Am Ceram Soc 1996, 79:2452-2457.
19. Kovar D., Thouless M.D., Halloran J.W. Crack deflection and propagation in layered silicon nitride/boron nitride ceramics. J Am Ceram Soc 1998, 81:1004-1012.
20. Ohji T., Shigegaki Y., Miyajima T., Kanzaki S. Fracture resistance behaviour of multilayered silicon nitride. J Am Ceram Soc 1997, 80:991-994.
21. Chartier T., Merle D., Besson J.L. Laminar ceramic composites. J Eur Ceram Soc 1995, 15:101-107.
22. Chartier T., Rouxel T. Tape cast alumina-zirconia laminates: processing and mechanical properties. J Eur Ceram Soc 1997, 17:299-308.
23. 3/SiC ceramics with improved mechanical behaviour. J Eur Ceram Soc 2000, 20:1771-1775.
24. Reynaud C., Thevenot F., Chartier T. Processing and microstructure of SiC laminar composites. Int J Refract Metals Hard Mater 2001, 19:425-435.
25. Ma J., Wang H., Weng L., Tan G.E.B. Effect of porous interlayers on crack deflection in ceramic laminates. J Eur Ceram Soc 2004, 24:825-831.
26. Reynaud C., Thévenot F., Chartier T., Besson J.L. Mechanical properties and mechanical behaviour of SiC dense-porous laminates. J Eur Ceram Soc 2005, 25:589-597.
27. Mistler R.E., Twiname E.R. Tape casting. Theory and practice 2000, The American Ceramic Society, USA.
28. 2 laminated composites. J Am Ceram Soc 1986, 69:191-192.
29. Tok A.I.Y., Boey F.T.C., Khor K.A. Tape casting of high dielectric ceramic composite substrates for microelectronic application. J Mater Proc Technol 1999, 89(90):508-512.
30. 3 slurries. J Eur Ceram Soc 2000, 20:1691-1697.
31. 5) multilayer composite prepared by tape casting. J Eur Ceram Soc 1999, 19:2111-2116.
32. Albano M.P., Garrido L.B. Influence of the slip composition on the properties of tape-cast alumina substrates. Ceram Int 2005, 31:57-66.
33. 2 laminate processed by tape casting: microstructure and mechanical properties' investigation. Intermetallics 2008, 16:758-768.
34. Biamino S., Liedtke V., Badini C., Euchberger G., Huertas Olivares I., Pavese M., et al. Multilayer SiC for thermal protection system of space vehicles: manufacturing and testing under simulated re-entry conditions. J Eur Ceram Soc 2008, 28:2791-2800.
35. Stavrinidis C., Tumino G., Caporicci M., Pradier A. European technology development efforts in the field of structures in preparation of future reusable space transportation systems. Proceedings of the 1st AIAA/IAF Symposium on Future Reusable Launch Vehicles 2002, 1830.
36. Hass D.D., Parrish P.A., Wadley H.N.G. Electron beam directed vapor deposition of thermal barrier coatings. J Vac Sci Technol, A 1998, 16:3396-3401.
37. Khor K.A., Dong Z.L., Gu Y.W. Plasma sprayed functionally graded thermal barrier coatings. Mater Lett 1999, 38:437-444.
38. Badini C., Fino P., Ortona A., Amelio C. High temperature oxidation of multilayered SiC processed by tape casting and sintering. J Eur Ceram Soc 2002, 22:2071-2079.
39. Pavese M., Fino P., Ortona A., Badini C. Potential of SiC multilayer for high temperature applications in oxidising environment. Ceram Int 2008, 34:197-203.
40. Specchia S., Civera A., Saracco G. In situ combustion synthesis of perovskite catalysts for efficient and clean methane premixed metal burners. Chem Eng Sci 2004, 59:5091-5098.
41. Biamino S., Fino P., Fino D., Russo N., Badini C. Catalyzed traps for diesel soot abatement: in situ processing and deposition of perovskite catalyst. Appl Catal B 2005, 61:297-305.
42. Parker W.J., Jenkins R.J., Butler C.P., Abbott G.L. Flash method of determining thermal diffusivity, heat capacity, and thermal conductivity. J Appl Phys 1961, 32:1679-1684.
43. Lewis J.A. Binder removal from ceramics. Annu Rev Mater Sci 1997, 27:147-173.
44. Stobierski L., Gubernat A. Sintering of silicon carbide. I. Effect of carbon. Ceram Int 2003, 29:287-292.