宋桂明, 周玉, 王玉金, 等. 固体火箭发动机喉衬材料[J]. 固体火箭技术, 1998, 21(2):51-55. (SONG Gui-ming, ZHOU Yu, WANG Yu-jin, et al. Throat materials for solid rocket motors[J]. Journal of Solid Rocket Technology, 1998, 21(2):51-55.)
|
D.L.Schmidt, K.E. Davidson, L S Theibet. Unique application of carbon-carbon composite material[J]. SAMPE,1999, 35(4):51-62.
|
苏君明. C/C复合材料喉衬的研究与发展[J]. 炭素科技, 2001, 11(1):6-11. (SU Jun-ming. Research and development of C/C throat insert material[J]. Carbon Science and technology, 2001, 11(1):6-11.)
|
苏君明. 高效高冲质比C/C喷管的应用与进展[J]. 新型炭材料, 1996, 11(3):18-23. (SU Jun-ming. Application and development of C/C nozzle with high specific thrust rate[J]. New Carbon Materials, 1996, 11(3):18-23.)
|
刘建军, 苏君明, 陈长乐. 炭/炭复合材料烧蚀性能影响因素分析[J]. 炭素, 2003, (2):15-19. (LIU Jian-jun, SU Jun-ming, CHEN Chang-le. Study on factors affecting ablative performance of C/C composites[J]. Carbon(Chinese), 2003, (2):15-19.)
|
黄海明, 杜善义, 吴林志, 等. C/C复合材料烧蚀性能分析[J]. 复合材料学报, 2001, 18(3):76-80. (HUANG Hai-ming, DU Shan-yi, WU Lin-zhi, et al. Analysis of the Ablation of C/C Composites[J]. Acta Material Composite Sinica, 2001, 18(3):76-80.)
|
HOU Xiao, CHENG Wen, Chen Ni. Preparation of a high performance carbon/carbon composite throat insert woven with axial carbon rods[J]. New Carbon Materials, 2013, 28(5):355-362.
|
王书贤, 陈林泉, 刘勇琼. C/C喉衬材料烧蚀试验方法研究[J]. 固体火箭技术, 2007, 30(2):170-172. (WANG Shu-xian, CHEN Lin-quan, LIU Yong-qiong. Investigation on ablative property test methods for C/C throat insert material[J]. Journal of Solid Rocket Technology, 2007, 30(2):170-172.)
|
苏君明, 周绍建, 李瑞珍, 等. 工程应用C/C复合材料的性能分析与展望[J]. 新型炭材料, 2015, 30(2):106-114. (SU Jun-ming, ZHOU Shao-jian, LI Rui-zhen, et al. A review of carbon-carbon composites for engineering applications[J]. New Carbon Materials, 2015, 30(2):106-114.)
|
苏君明, 谢乔, 冯婧, 等. 喉衬用石墨材料的性能和功能评价[J]. 固体火箭技术, 2015, 38(4):554-561. (SU Jun-ming, XIE Qiao, FENG Jing, et al. The evaluation of performance and function of graphite material for throat insert[J]. Journal of Solid Rocket Technology, 2015, 38(4):554-561.)
|
张名大. 热解石墨栅极[J]. 炭素, 1980(1):1-8. (ZHANG Ming-da. Grid of pyrolytic graphite[J]. Carbon(Chinese)1980(1):1-8.)
|
Borie V. An aerotheramal chemical analysis of carbon-carbon nozzle regression in solid-propellant rocket motor[R]. AIAA-88-3346.
|
Thakre P, Yang V. A comprehensive model to predict and mitigate the erosion of carbon-carbon/graphite rocket nozzles[R]. AIAA 2007-5777.
|
Daniele Bianchi, Francesco Nasuti, Emanuele Martelli. Coupled analysis of flow and surface ablation in carbon-carbon rocket nozzles[R]. AIAA 2008-3912.
|
D.E. Whitney, K.P. Hennessey. Development of an alternate nozzle for the MK 111 tomahawk booster rocket motor[R]. AIAA 92-3555.
|
G C Lamere. MX first stage nozzle development[C]. AO/A103844.
|
M. Bussiere. M. Prel. Ariane V solid rocket booster nozzle development status[R]. AIAA-94-3063.
|
刘建军, 李铁虎, 郝志彪. 喉衬热环境与碳/碳复合材料的烧蚀[J]. 宇航材料工艺, 2005(1):42-48. (LIU Jian-jun, LI Tie-hu, HAO Zhi-biao. Throat thermal ambient and ablation of C/C composites[J]. Aerospace Material Process, 2005(1):42-48.)
|
冉红星, 崔红, 郝志彪, 等. 碳基体结构状态对C/C复合材料抗烧蚀性能的影响[J]. 炭素, 2002(4):20-25. (RAN Hong-xing, CUI Hong, HAO Zhi-biao, et al. Influence of carbon matrix structure on antiablative performances of C/C composites[J]. Carbon(Chinese)2002(4):20-25.)
|
苏君明, 邵海成, 肖志超, 等. 低烧蚀率针刺炭纤维炭/炭复合材料喉衬的制备与性能研究[J]. 炭素技术, 2013, 32(6):A1-A5. (SU Jun-ming, SHAO Hai-cheng, XIAO Zhi-chao, et al. Preparation and properties of needling carbon/carbon composites throat with low ablation rate[J]. Carbon Techniques, 2013, 32(6):A1-A5.)
|