Guo W D. Study of increasing the burning rate of solid propellants by adding fast burning energetic materials[J]. Journal of Propulsion Technology,1998,19(3): 89-93.
[2]
Sayles D C. Embedded explosives as burning rate accelerators for solid propellants: USP5015310 ,1991.5.14.
[3]
David C S. Methods of increasing the burning rate enhancement by mechanical accelerators: USP4812179 ,1989.3.14.
[4]
Frolov Y V,Korostelev V G. Combution of gas-permeable porous systems[J]. Propellants,Explosives,Pyrotechnics,1989,14: 140-149.
[5]
郭效德,李凤生,宋洪昌,等. 新型高燃速推进剂的催化燃烧性能[J]. 推进技术,2007,28(2): 220-224. GUO Xiao-de,LI Feng-sheng,SONG Hong-chang,et al. Catalytic combustion properties of a new high burning rate propellant[J]. Journal of Propulsion Technology,2007,28(2): 220-224.
[6]
冉秀伦,杨荣杰,王国强. 快燃物ACP在丁羟复合固体推进剂中的应用[J]. 火炸药学报,2006,29 (5): 42-45. RAN Xiu-lun,YANG Rong-jie,WANG Guo-qiang. Application of fast-burning energetic compound ACP in HTPB composite propellants[J]. Chinese Journal of Explosives & Propellants,2006,29(5): 42-45.
[7]
廖林泉,覃光明,李笑江,等. 用ACP提高硝胺改性双基推进剂的燃速[J]. 推进技术,2005,26(1): 84-88. LIAO Lin-quan,QIN Guang-ming,LI Xiao-jiang,et al. Increasing the burning rate of nitramine modified double-base propellant with ACP[J]. Journal of Propulsion Technology,2005,26(1): 84-88.
[8]
李晓东,何吉宇,杨荣杰,等. 多孔超高燃速推进剂代料的双螺杆混合工艺初探[J].宇航学报,2003,24(4): 429-432. LI Xiao-dong,HE Ji-yu,YANG Rong-jie,et al. Study on twin-screw extrusion technology of porous ultra high burning rate propellant substitutes[J]. Journal of Astronautics,2003,24(4): 429-432.
[9]
Fischer T S,Boehnlein-Mauss J,Eberhardt A,et al. Burning characteristics of foamed polymer bonded propellants //33rd International Annual Conference of ICT,2002,Karlsruhe,Germany. 139/1-139/14.
[10]
Farinaccio R,Lessard P. Experimental investigation of high burn rate propellant for use in nozzleless boosters . AIAA2000-3320,2000.
[11]
蔺向阳,程向前,潘仁明,等. 微气孔球形药常压燃烧特征[J]. 火炸药学报,2005,28(4): 68-71. LIN Xiang-yang,CHENG Xiang-qian,PAN Ren-ming,et al. Combustion property of oblate propellant with micropores in air[J]. Chinese Journal of Explosives & Propellants,2005,28(4): 68-71.
[12]
冉秀伦,杨荣杰. 高燃速推进剂研制现状分析[J]. 飞航导弹,2006(9): 44-50. RAN Xiu-lun,YANG Rong-jie. A survey of development of propellants with high burning rate[J]. Winged Missiles Journal,2006(9): 44-50.
[13]
廖林泉,李笑江,覃光明. 提高固体推进剂燃速方法述评[J]. 飞航导弹,2004(2): 39-41. LIAO Lin-quan,LI Xiao-jiang,QIN Guang-ming. Review of improving the solid propellant burning rate[J]. Winged Missiles Journal,2004(2): 39-41.
[14]
刘继华. 火药的物理化学性质[M]. 北京: 北京理工大学出版社,1997. LIU Ji-hua. Physics and Chemistry Properties of Propellant[M]. Beijing: Beijing Institute of Press,1997.
