[1] Fitzer E, Manocha L M. Carbon Reinforcements and Carbon/Carbon Composites. Berlin: Springer, 1998: 250 - 319. [2] Savage. G. Carbon-Carbon Composites. London: Chapman & Hall. 1993: 31 - 357. [3] Boury D, Filipuzzi L. Sepcarb ? Materials for Solid Rocket Booster Nozzle Components. In: 37th AIAA/ASME/SAE/ASEE joint propulsion conference, Salt Lake City, Utah, US 2001, AIAA - 2001 - 3438. [4] Boury D, Munoz M, Albert A, et al. Ariane 5 SRM nozzle evolution. In: 38th AIAA/ASME/SAE/ASEE joint propulsion conference joint propulsion conference, Indianapolis, IN, US 2002, AIAA - 2002 - 4193. [5] Lacombe A, Lacoste M, Pichon T. 3D Novoltex? and Naxeco? Carbon-Carbon Nozzle Extensions; Matured, Industrial and Available Technologies to Reduce Programmatic and Technical Risks and to Increase Performance of Launcher Upper Stage Engines. In: 44th AIAA/ASME/SAE/ASEE joint propulsion conference & exhibit, Hartford, CT, US 2008, AIAA - 2008 - 5236. [6] Berdoyes M. Snecma Propulsion Solide Advanced Technology SRM Nozzles. History and Future. In: 42nd joint propulsion conference & exhibit, Sacramento, CA, US 2006, AIAA - 2006 - 4596. [7] 崔 红, 苏君明, 李瑞珍, 等. 添加难熔金属碳化物提高 C/C 复合材料抗烧蚀性能的研究. 西北工业大学学报, 2000, 18(4): 669 - 673. [8] Choury J J. Carbon-Carbon Materials for Nozzles of Solid Propellant Rocket Motors. In: 12th propulsion conference, Palo Alto, CA 1976, AIAA - 76 - 609. [9] Shen X T, Li K Z, Li H J, et al. Microstructure and ablation properties of zirconium carbide doped carbon/carbon composites. Carbon, 2010, 48(2): 344 - 351. [10] 李翠艳, 李克智, 欧阳海波, 等 (LI Cui-Yan, et al) . HfC 改性炭 / 炭复合材料的烧蚀性能.稀有金属材料与工程 (Rare Metal Mat. Eng. ), 2006, 35 ( Suppl. 2 ): 365 - 368. [11] 李淑萍, 李克智, 郭领军, 等 ( LI Shu-Ping, et al ). HfC 改性 C/C 复合材料整体喉衬的烧蚀性能研究. 无机材料学报 ( Journal of Inorganic Materials ), 2008, 23(6): 1155 - 1158 ﹒ [12] Gordon S, McBride B J. Computer Program for Calculation of Complex Chemical Equilibrium Compositions and Applications I: Analysis. NASA Lewis Research Center: N ASA Reference Publication, 1994: 25 - 32. [13] Thakre P, Yang V. Chemical erosion of carbon-carbon/graphite nozzles in solid-propellant rocket motors. J. Propul. Power, 2008, 24(4): 822 - 833. [14] Bianchi D, Nasuti F, Martelli E. Coupled Analysis of Flow and Surface Ablation in Carbon-Carbon Rocket Nozzles. In: 40th thermophysics conference. Seattle, Washington 2008, AIAA - 2008 - 3912. [15] Guo W M, Xiao H N, Yasuda E, et al. Oxidation kinetics and mechanisms of a 2D-C/C composite. Carbon, 2006, 44(15): 3269 - 3276. [16] Lachaud J, Aspa Y, Vignoles G L. Analytical modeling of the steady state ablation of a 3D C/C composite. Int. J. Heat. Mass. Tran. , 2008, 51(9/10): 2614 - 2627. [17] Cho D, Yoon B I. Microstructural interpretation of the effect of various matrices on the ablation properties of carbon-fiber-reinforced composites. Compos. Sci. Tech nol. , 2001, 61(2): 271 - 280. [18] Lee Y J, Joo H J. Investigation on ablation behavior of CFRC composites prepared at different pressure. Compos. Part A, 2004, 35(11): 1285 - 1290. [19] Savvatimskiy A I. Measurements of the melting point of graphite and the properties of liquid carbon (a review for 1963-2003). Carbon, 2005, 43(6): 1115 - 1142. |