Advances on ultra-high temperature materials

Guti Huojian Jishu/Journal of Solid Rocket Technology

Volumn 28, Issue 4, 2005, Pages 289-294

  Han, Jie Cai ^a   Hu, Ping ^a   Zhang, Xing Hong ^a   Meng, Song He ^a  

^a HARBIN INSTITUTE OF TECHNOLOGY   (China)

Author keywords

Carbon carbon composites; Ceramic composites; Refractory metals; Ultra high temperature materials

Indexed keywords

APPLICATIONS; CARBON CARBON COMPOSITES; CERAMIC MATRIX COMPOSITES; HIGH TEMPERATURE PROPERTIES; PROPULSION; REENTRY; REFRACTORY METALS; ROCKETS;

CROSSOVER FLIGHT; REENTRY FLIGHT; SUPERSONIC FLIGHT; ULTRAHIGH TEMPERATURE MATERIALS;

COMPOSITE MATERIALS;

EID: 32344446528     PISSN: 10062793     EISSN: None     Source Type: Journal    
DOI: None     Document Type: Article

References (47)

1. Upadhya K, Yang J-M, Hoffmann W P. Materials for ultra-high temperature structural applications [J]. Am. Ceram. Soc. Bull, 1997, 76(12): 51-56.
2. William G Fahrenholtz, Gregory E Hilmas. NSF-AFOSR joint workshop on future ultra-high temperature materials [R]. NSF Grant DMR-0403004.
3. Bronson A, Ma Y T, Mutso R. Compatibility of refractory metal boride/oxide composites at ultra-high temperatures [J]. J. Electrochem. Soc., 1992, 139(11): 3183-3196.
4. Opeka M, Talmy I G, Wuchina E J, Zaykoski J A, Causey S J. Mechanical, thermal, and oxidation properties of refractory hafnium and zirconium compounds [J]. J. Eur. Ceram. Soc., 1999, 19(13-14): 2405-2414.
5. Wang C R, Yang J M, Hoffmann W. Thermal stability of refractory carbide/boride composites [J]. Mater. Chem. Phys., 2002, 74(3): 272-274.
6. 2 plus 20 v/o SiC composite [J]. J. Electrochem. Soc., 1975, 122(9): 1249-1254.
7. 2 [J]. Ceram. Bull, 1973, 52(8): 612-616.
8. Levine S R, Opila E J, Halbig M C, Riser J D, Singh M, Salem J A. Evaluation of ultra-high temperature ceramics for aeropropulsion use [J]. J. Eur. Ceram. Soc., 2002, 22(14, 15): 2757-2767.
9. Opeka M M, Talmy I G, Zaykoski J A. Oxidation-based materials selection for 2000°C + hypersonic aerosurfaces: Theoretical considerations and historical experience[J]. J. Mater. Sci., 2004, 39(19): 5887-5904.
10. Goujard S, et al. The oxidation behaviour of two and three dimensional C/SiC thermostructural materials protected by chemical vapour deposition polylayers coatings [J]. J. Mater. Sci., 1994, 29(20): 6212-6220.
11. Bertrand S, Pailler R, Lamon J. SiC/SiC minicomposites with nanoscale multilayered fiber coatings [J]. Composites Science and Technology, 2001, 61(3): 363-367.
12. DiCarlo J A, Yun H M, Morscher G N, Bhatt R T. Progress in SiC/SiC ceramic composite development for gas turbine hot-section components under NASA EPM and UEET programs [J]. Am. Soc. Mec. Engi., 2002, (4): 39-45.
13. Suyama S, Kameda T, Itoh Y. Evaluation of microstructure for SiC/SiC composites [J]. Inter. J. Mater. Pro. Tech., 2001, 16(1-3): 232-238.
14. Song Gui Ming, Yu Zhou, Wang Yu Jin. Effect of carbide particles on the ablation properties of tungsten composites [J]. Mater. Character, 2003, 50: 293-303.
15. Song G M. Microstructure-properties and thermal shock behavior of TiC/W and ZrC/W composites [D]. Ph. D. thesis, Harbin: Harbin Institute of Technology, 1999: 68-79.
16. Alan H, Rosenstein. Overview of research on aerospace metallic structural materials [J]. Materials Science and Engineering A, 1991, 143: 31-41.
17. 2 in-situ composites at elevated temperatures [J]. Intermetallics, 2003, 11: 787-794.
18. Yoko Y M, Yoshikazu Ro, Nakazawa S, Harada H. High temperature strength of Ir-based refractory superalloys [J]. J. Jap. Ins. Met., 2000, 64(11): 1068-1075.
19. Fischer B, Lupton D F, Freund D. Stress-rupture strength of rhenium at very high temperatures [C]. TMS Annual Meeting, Rhenium and Rhenium Alloys, 1997: 311-320.
20. Chazen M L. Materials property test results of rhenium[C]. TMS Annual Meeting, Rhenium and Rhenium Alloys, 1997: 301-308.
21. Sherman A J, Tuffias R H, Fortini A J, Williams B E. Impact of the mechanical properties of rhenium on structural design[C]. TMS Annual Meeting, Rhenium and Rhenium Alloys, 1997: 291-300.
22. Diaz J J. Pure rhenium metal[J]. IEEE Potentials, 1996, 15(1): 37-39.
23. Ohriner E K. Rhenium and iridium[C]. TMS Annual Meeting, Rhenium and Rhenium Alloys, 1997: 409-423.
24. Sherman A J, Tuffias R H, Kaplan R B. Properties and applications of rhenium produced by CVD[J]. JOM, 1991, 43(7): 20-23.
25. Kim K T, Wang J J, Welsch G. Chemical vapor deposition (CVD) of rhenium [J]. Mater. Let., 1991, 12(1,2): 43-46.
26. Reed B, Biaglow J, Schneider S. Iridium-coated rhenium radiation-cooled rockets [C]. TMS Annual Meeting, Rhenium and Rhenium Alloys, 1997: 443-457.
27. Duriez C. Rhenium oxidation by steam at high temperatures [J]. Oxidation of Metals, 2004, 61(1,2): 49-67.
28. Tuffias R. State of the art fabrication processes for iridium/rhenium thrust chambers[C]. TMS Annual Meeting, Rhenium and Rhenium Alloys, 1997: 251-260.
29. 2]-SiC composites [J]. J. Am. Ceram. Soc., 2000, 83(9): 2330-2332.
30. Ohlhorst C W, Vaughn W L. Arc jet results on candidate high temperature coatings for NASA's NGLT refractory composite leading edge task[R]. NASA/Langley Research Center.
31. Bargeron C B, Benson R C, Newman R W. Oxidation mechanisms of hafnium carbide and hafnium diboride in the temperature range 1400 to 2100°C [J]. Johns Hopkins APL Technical Digest (Applied Physics Laboratory), 1993, 14(1): 29-36.
32. Bargeron C B, Benson R C. X-ray microanalysis of a hafnium carbide film oxidized at high temperature [J]. Surface and Coatings Technology, 1998, 36(1): 111-115.
33. Holcomb G R, Pierre G R. Application of a counter-current gaseous diffusion model to the oxidation of hafnium carbide at 1200 to 1530°C [J]. Oxidation of Metals, 1993, 40(1,2): 109-118.
34. Holcomb G R. Countercurrent gaseous diffusion model of oxidation through a porous coating [J]. Corrosion (Houston), 1996, 52(7): 531-539.
35. Courtright E L, Prater J T, Holcomb G R, Pierre G R, Rapp R A. Oxidation of hafnium carbide and hafnium carbide with additions of tantalum and praseodymium [J]. Oxidation of Metals, 1991, 36(5,6): 423-437.
36. Ron Loehman, Dale Zschiesche. Ultra-high temperature ceramics for hypersonic vehicle applications [R]. Ronald E., Loehman, Sandia National Laboratories, Ceramic Materials Dept. Albuquerque, N. Mex.
37. Gasch M, Ellerby D, Irby E, Beckman S, Gusman M, Johnson S. Processing, properties and arc jet oxidation of hafnium diboride/silicon carbide ultra-high temperature ceramics [J]. Journal of Materials Science, 2004, 39(19): 5925-5937.
38. Levine S R, Opila E J. Tantalum addition to zirconium diboride for improved oxidation resistance [R]. NASA/TM2003-212483.
39. Talmy I G, et al. High temperature corrosion and materials chemistry III[J]. Electrochem. Soc., 2001, 12: 144-149.
40. Varshal B G. A structural model of immiscibility of silicate glass-forming melts[J]. Glass Phys. Chem., 1993, 19: 218-225.