[1] Naslain R. High Temperature Ceramic Matrix Composite, London: Woodhead Publications, 1993. 735--778. [2] Nannetti C A, Riccardi B, Ortona A. Journal of Nuclear Materials, 2002, 307-311 (2): 1196--1199. [3] 张立同, 成来飞, 徐永东. 航空制造技术, 2003, (1): 24--32. [4] 闫联生, 邹武. 固体火箭技术, 1998, 21 (1): 54--58. [5] Zheng G B, Sano H, Uchiyama Y, et al. J. Mater. Sci., 1999, 34 (4): 827--834. [6] 闫联生, 王涛, 邹武, 等. 宇航材 料工艺, 1999, 29 (3): 38--41. [7] Lackey J, Hanigofsky J A, Freeman G B, et al. J. Am. Ceram. Soc., 1995, 78 (6): 1564--1570. [8] Inghels E, Lamon J. J. Mater. Sci., 1991, 26 (11): 5403--5410. [9] Kaya H. Journal of Composite Science & Technology, 1999, 59 (3): 861--872. [10] Trabandt U, Wulz H G, Schmid T. Journal of Key Engineering Materials, 1999, 164-165 (2): 445--450. [11] Loumagne F, Langlais F, Naslain R, et al. Thin Solid Films, 1995, 254 (1): 75--82. [12] 尹洪峰, 徐永东, 成来飞, 等(YIN Hong-Feng, et al). 硅酸盐学报(Journal of The Chinese Ceramic Society), 2000, 28 (5): 437--440. |