Ablation behavior and mechanism of 3D C/ZrC composite in oxyacetylene torch environment

Composites Science and Technology

Volumn 71, Issue 11, 2011, Pages 1392-1396

  Zhao, Dan ^a   Zhang, Changrui ^a   Hu, Haifeng ^a   Zhang, Yudi ^a  

^a NATIONAL UNIVERSITY OF DEFENSE TECHNOLOGY   (China)

Author keywords

A. Carbon fiber; A. Ceramic matrix composites (CMCs); A. Zirconium carbide; B. Ablation behavior

Indexed keywords

CARBIDES; CERAMIC MATRIX COMPOSITES; HEAT FLUX; ZIRCONIA;

ABLATION PROPERTIES; B. ABLATION BEHAVIOR; CARBON FIBER REINFORCED; CERAMIC-MATRIX COMPOSITES (CMCS); CONFIGURATIONAL STABILITY; SURFACE TEMPERATURES; TEMPERATURE AND PRESSURES; ZIRCONIUM CARBIDE;

ABLATION;

EID: 79960224469     PISSN: 02663538     EISSN: None     Source Type: Journal    
DOI: 10.1016/j.compscitech.2011.05.005     Document Type: Article

References (21)

1. Kontinos DA, Gee K, Prabhu DK. Temperature constraints at the sharp leading edge of a crew transfer vehicle. AIAA 2001-2886; 2001.
2. Savino R., Fumo M.D.S., Paterna D., Serpico M. Aerothermodynamic study of UHTC-based thermal protection systems. Aerosol Sci Technol 2005, 9:151-160.
3. Kolodziej P, Salute J, Keese DL. First flight demonstration of a sharp ultra-high temperature ceramic nosetip. NASA TM-112215; 1997.
4. Loomis M, Plamer G. Pre-flight CFD analysis of art jet and flight environments for the SHARP-B2 flight experiment. AIAA 2001-0982; 2001.
5. 2-SiC composites under hypersonic re-entry conditions. J Eur Ceram Soc 2010, 30:2313-2321.
6. 2-SiC ultra high temperature ceramics under simulated atmospheric re-entry conditions. Compos Sci Technol 2008, 68:1718-1726.
7. Yin J., Zhang H., Xiong X., Huang B., Zuo J. Ablation properties of carbon/carbon composites with tungsten carbide. Appl Surf Sci 2009, 255:5036-5040.
8. 2-SiC composites at 2200°C. Compos Sci Technol 2008, 68:799-806.
9. Zhang X.H., Hu P., Han J.C., Xu L., Meng S.H. The addition of lanthanum hexaboride to zirconium diboride for improved oxidation resistance. Scripta Mater 2007, 57:1036-1039.
10. 2 composites by precursor infiltration and pyrolysis process. Ceram Int 2010, 36:1011-1016.
11. 2-SiC ultra high temperature ceramic composites. Mater Sci Eng 2009, 524:129-133.
12. Tong Q., Shi J., Song Y., Guo Q., Liu L. Resistance to ablation of pitch-derived ZrC/C composites. Carbon 2004, 42:2495-2500.
13. Zhao D., Zhang C., Hu H., Zhang Y., Wang J. A simple way to prepare precursors for zirconium carbide. J Mater Sci 2010, 45:6401-6405.
14. Hu H., Chen Z., Xiao J., Zheng W. Synthesis and characterization of polysilazane precursor. J Mater Sci Lett 1999, 18:1271-1272.
15. Shen X.T., Li K.Z., Li H.J., Fu Q.G., et al. The effect of zirconium carbide on ablation of carbon/carbon composites under an oxyacetylene flame. Corros Sci 2011, 53:105-112.
16. 2 from the oxidation of ZrC on ablation of ZrC modified carbon/carbon composites. J Inorg Mater 2009, 24(5):943-947. in Chinese.
17. Shen X.T., Li K.Z., Li H.J., Du H.Y., et al. Microstructure and ablation properties of zirconium carbide doped carbon/carbon composites. Carbon 2010, 48(2):344-351.
18. Wang Q.K., Hu H.F., Chen Z.H. Effect of ZrC content on the microstructure and properties of 2D C/SiC-ZrC composites via precursor infiltration and pyrolysis. J Aeronaut Mater 2009, 29(3):72-76. [in Chinese].
19. Sun W., Xiong X., Huang B.Y., Li G.D., et al. ZrC ablation protective coating for carbon/carbon composites. Carbon 2009, 47(14):3368-3371.
20. Wang Y.G., Zhu X.J., Zhang L.T., Cheng L.F. Reaction kinetics and ablation properties of C/C-ZrC composites fabricated by reactive melt infiltration. Ceram Int 2011, 37(4):1277-1283.
21. Fang D., Chen Z., Song Y., Sun Z. Morphology and microstructure of 2.5 dimension C/SiC composites ablated by oxyacetylene torch. Ceram Int 2009, 35:1249-1253.