[1] Ho S Y. Thermomechanical properties of rocket propellants and correlation with cookoff behaviour [J]. Propellants, Explosives, Pyrotechnics, 1995, 20(4): 206-214. [2] Ho S Y, Ferschl T, Foureur J. Correlation of cook-off behavior of rocket propellants with thermo-mechanical and thermochemical properties, ADA274983[R]. AU: DSTO, 1993. [3] Sumrall T S. Large scale fast cook-off sensitivity results of a melt castable general purpose insensitive high explosive [J]. Propellants, Explosives,Pyrotechnics, 1999, 24(2): 61-64. [4] Caro R I, Bellerby J M. Behavior of hydroxyl-terminated polyether (htpe) composite rocket propellants in slow cook-off [J]. International Journal of Energetic Materials and Chemical Propulsion, 2008, 7(3): 171-185. [5] Komai I, Sato W. Reaction mechanism in slow cook-off test of GAP-AP propellants [C]∥Insensitive Munitions and Energetic Materials Technology Symposium (IMEMTS). Bristol, UK: Insensitive Munitions European Manufacturers Group, 2006:24-28. [6] 秦能,裴江峰,王明星. 一种RDX-CMDB推进剂危险性能研究[J]. 含能材料, 2011, 19(6): 725-729. QIN Neng, PEI Jiang-feng, WANG Ming-xing. Hazard property of the RDX-CMDB propellant [J]. Chinese Journal Energetic Materials,2011,19(6): 725-729. (in Chinese) [7] 秦能,裴江峰. 某种RDX-CMDB螺压推进剂刺激-响应特性试验研究[C]∥ 中国化学会第五届全国化学推进剂学术会议. 大连: 中国化学会,2011. QIN Neng, PEI Jiang-feng. Stimulate-response characteristic test research of a screw press propellant of RDX-CMDB [C]∥The 5th National Conference on Chemical Propellant of Chinese Chemistry. Dalian: Chinese Chemical Society, 2011. (in Chinese) [8] 胥会祥,赵凤起,庞维强,等. 含FOX-12的高燃速HTPB推进剂性能[J]. 固体火箭技术, 2011, 34(6): 745-749. XU Hui-xiang, ZHAO Feng-qi, PANG Wei-qiang, et al. Properties of high burning rate HTPB propellant containing FOX-12 [J]. Journal of Solid Rocket Technology, 2011, 34(6): 745-749. (in Chinese) [9] 丁黎,王琼,张腊莹,等. 高固含量对改性双基推进剂的热安全特性影响[C]∥第二届全国危险物质与安全应急技术研讨会. 四川成都: 中国化学会,2013. DING Li, WANG Qiong, ZHANG La-ying, et al. Thermal safety characteristics influence of modified double-base propellant with different high solid contents [C]∥The 2nd National Hazardous Materials and Safety Emergency Technical Seminar. Chengdu, Sichuan: Chinese Chemical Society,2013. (in Chinese) [10] 李高春,袁书生,原渭兰,等. 固体火箭发动机的热响应研究 [J]. 弹箭与制导学报,2005, 25(4): 371-373. LI Gao-chun, YUAN Shu-sheng, YUAN Wei-lan, et al. Investigation on the thermal response of solid rocket motor [J]. Journal of Projectiles, Rockets, Missiles and Guidance, 2005, 25(4): 371-373. (in Chinese) [11] 原渭兰,潘浪. 一种舰载导弹固体火箭发动机烤燃过程的数值计算 方法[J]. 舰船科学技术,2009, 31(7): 129-132. YUAN Wei-lan, PAN Lang. An numerical calculation method on cook-off of solid rocket motor of ship-based missiles [J]. Ship Science and Technology, 2009, 31(7): 129-132. (in Chinese) [12] Zhou X U, Jackson T L, Buckmaster J. Oscillations in propellant flames with edges [J]. Combustion and Flame, 2003, 133(1/2): 157-168. [13] Hegab A, Jackson T L, Buckmaster J, et al. Nonsteady burning of periodic sandwich propellants with complete coupling between the solid and gas phases [J]. Combustion and Flame, 2001, 125(1): 1055-1070. [14] Wang X, Jackson T L, Massa L. Numerical simulation of heterogeneous propellant combustion by a level set method [J]. Combustion Theory and Modelling, 2004, 8(2): 227-254. [15] 杨世铭,陶文铨. 传热学[M]. 北京:高等教育出版社,2006: 558-560. YANG Shi-ming, TAO Wen-quan. Heat transfer [M].Beijing: Higher Education Press, 2006: 558-560. (in Chinese) [16] 陈广南,张为华. 固体火箭发动机撞击与热安全性分析[M]. 北京: 国防工业出版社, 2008: 196-197. CHEN Guang-nan, ZHANG Wei-hua. Safety analyses for solid rocket motors under insults of impact and heat[M].Beijing: National Defense Industry Press,2008: 196-197. (in Chinese) [17] Kim K H, Kim C K, Yoo J C. Test-based thermal decomposition simulation of AP/HTPB and AP/HTPE propellants [J]. Journal of Propulsion and Power, 2011, 27(4): 822-827. [18] Gwak M, Jung T, Yoh J J. Friction-induced ignition modeling of energetic materials [J]. Journal of Mechanical Science and Technology, 2009, 23(7): 1779-1787. |