[1]黄 蒙,丁 黎,常 海,等.HTPB/Al/AP/RDX复合推进剂组元之间相互作用研究[J].火炸药学报,2020,43(2):203-207,212.[doi:10.14077/j.issn.1007-7812.201907034]
 HUANG Meng,DING Li,CHANG Hai,et al.Study on Interaction between Component for HTPB/Al/AP/RDX Composite Propellant[J].,2020,43(2):203-207,212.[doi:10.14077/j.issn.1007-7812.201907034]
点击复制

HTPB/Al/AP/RDX复合推进剂组元之间相互作用研究

参考文献/References:

[1] 王海波. 丁羟四组元复合推进剂固体化体系研究[D]. 长沙:湖南大学, 2007.
WANG Hai-bo. Study on curing system of four-components HTPB composite propellants[D]. Changsha: Hunan University, 2007.
[2]张翠芳, 吴晓青, 张文才, 等.丁羟推进剂的应用发展[J]. 天津化工, 2002, 22(2):12-14.
ZHANG Cui-fang, WU Xiao-qing, ZHANG Wen-cai, et al. The application and devolopment of Hydroxy-terminated-polybutadiene propellant[J]. Tianjin Chemical Industry, 2002, 22(2):12-14.
[3]张海燕, 美军在伊拉克战争中使用的固体推进剂和战斗部[J]. 火炸药学报, 2004, 27(1):49-52.
ZHANG Hai-yan. Solid propellants and warheads practised by US forces in war on Iraq[J]. Chinese Journal of Explosives & Propellants(Huozhayao Xuebao), 2004, 27(1):49-52.
[4]裴庆, 赵凤起, 罗阳, 等. 固体推进剂燃速测试技术研究进展[J]. 火炸药学报, 2015, 38(3):9-14
PEI Qing, ZHAO Feng-qi, LUO Yang, et al. Research progress in the burning rate/measurement technology of solid propellants[J]. Chinese Journal of Explosives & Propellants(Huozhayao Xuebao), 2015, 38(3): 9-14.
[5]孙伟, 胡林俊, 魏子力. 高固体含量高强度丁羟推进剂工艺调节技术[C]∥中国宇航学会固体火箭推进第22届年会论文集(推进剂分册). 成都:中国宇航学会固体推进专业委员会,2005:133-135.
[6]MILLER M S, HOLMES H E. Subatmospheric burning rates and critical diameters for AP/HTPB propellant[J]. Journal of Propulsion and Power, 1990,6(5):671-672.
[7]庞爱民, 王北海. 丁羟聚氨酯弹性体结构与力学性能的关系综述[J]. 推进技术,1993, 14(5):53-58.
PANG Ai-ming, WANG Bei-hai. Relationship between the structure and the mechanical properties of HTPB[J]. Journal of Propulsion Technology, 1993, 14(5):53-58.
[8]陈沛, 赵凤起, 阴翠梅. RDX/AP/HTPB推进剂热分解特性研究[J]. 固体火箭技术, 2002, 25(2):52-55.
CHEN Pei, ZHAO Feng-qi, YIN Cui-mei. Study on the thermal decomposition behavior of RDX/AP/HTPB propellant[J]. Journal of Solid Rocket Technology, 2002, 25(2):52-55.
[9]赵凤起, 陈沛, 李上文. 燃速调节剂对RDX/AP/HTPB推进剂热分解的影响 [J]. 推进技术, 2003, 24(1):80-82.
ZHAO Feng-qi, CHEN Pei, LI Shang-wen. Effect of the burning rate regulator on the thermal behavior of RDX/AP/HTPB propellant[J]. Journal of Propulsion Technology, 2003, 24(1):80-82.
[10]施震灏, 刘子如, 陈智群. DSC-FTIR联用研究HTPB/AP和HTPB/AP/Al体系的热分解[J]. 含能材料, 2007, 15(2):105-108.
SHI Zhen-hao, LIU Zi-ru, CHEN Zhi-qun. Thermal decomposition of HTPB/AP and HTPB/AP/Al studied by DSC-FTIR[J]. Chinese Journal of Energetic Materials, 2007, 15(2): 105-108.
[11]朱立勋, 梁蓓, 刘晋湘, 等. 铝形貌对丁羟推进剂燃速特性的影响[J]. 含能材料, 2017, 25(10):799-803.
ZHU Li-xun, LIANG Bei, LIU Jin-xiang, et al. Effect of aluminum morphology on buring rate characteristics of HTPB propellant[J]. Chinese Journal of Energetic Materials, 2017, 25(10):799-803.
[12] 赵佳辰, 焦清介, 郭学永. AP对RDX热稳定性及AP/RDX爆轰性能的影响[J]. 火炸药学报, 2019, 42(4):380-384.
ZHAO Jia-chen, JIAO Qing-jie, GUO Xue-yong. Effect of AP on the thermal stability of RDX and detonation performance of AP/RDX[J]. Chinese Journal of Explosives & Propellants(Huozhayao Xuebao), 2019, 42(4):380-384.
[13]刘子如. 含能材料热分析[M]. 北京:国防工业出版社, 2008.
[14]刘中兵, 汪亮, 胡春波. HTPB推进剂高压燃烧特性研究[J].固体火箭技术,2010,33(3):302-306.
LIU Zhong-bing, WANG Liang, HU Chun-bo. Study on burning characteristics of HTPB propellants under high pressure[J]. Journal of Solid Rocket Technology, 2010, 33(3):302-306.
[15]廖林泉, 胥会祥, 李勇宏, 等. HTPB推进剂危险性实验研究[J]. 火炸药学报, 2010, 33(4):28-43.
LIAO Lin-quan, XU Hui-xiang, LI Yong-hong, et al. Experimental study on hazard of HTPB propellants[J]. Chinese Journal of Explosives & Propellants(Huozhayao Xuebao), 2010, 33(4):28-43.

相似文献/References:

[1]何卫东,董朝阳.高分子钝感发射药的低温感机理[J].火炸药学报,2007,30(1):9.
[2]张 昊,彭 松,庞爱民,等.NEPE推进剂老化过程中结构与力学性能的关系[J].火炸药学报,2007,30(1):13.
[3]路向辉,曹继平,史爱娟,等.表面处理芳纶纤维在丁羟橡胶中的应用[J].火炸药学报,2007,30(1):21.
[4]李春迎,王 宏,孙 美,等.遥感FTIR光谱技术在固体推进剂羽焰测试中的应用[J].火炸药学报,2007,30(1):28.
[5]杜美娜,罗运军.RDX表面能及其分量的测定[J].火炸药学报,2007,30(1):36.
[6]王国栋,刘玉存.神经网络在炸药晶体密度预测中的应用[J].火炸药学报,2007,30(1):57.
[7]周诚,黄新萍,周彦水,等.FOX-7的晶体结构和热分解特性[J].火炸药学报,2007,30(1):60.
[8]张秋越,孟子晖,肖小兵,等.用分子烙印聚合物吸附溶液中的TNT[J].火炸药学报,2007,30(1):64.
[9]崔建兰,张 漪,曹端林.三羟甲基丙烷三硝酸酯的热分解性能[J].火炸药学报,2007,30(1):71.
[10]李进华,孙兆懿.四氧化二氮胶体饱和蒸气压的测试及分析[J].火炸药学报,2007,30(1):74.

备注/Memo

收稿日期:2019-07-24; 修回日期:2019-11-25
基金项目:国家自然科学基金(No.21805223; No.21805226)
作者简介:黄蒙(1995-),女,硕士研究生,从事含能材料热性能研究。E-mail:zitian1234@163.com
通信作者:常海(1962-),男,研究员,从事含能材料性能研究。E-mail:chang_hai_2011@126.com

更新日期/Last Update: 2020-05-13


@Copyright 西安近代化学研究所(中国兵器工业第204研究所)  陕ICP备14002633号-2
地址:西安市18号信箱《火炸药学报》编辑部   联系电话:029-88291297   邮箱:hzyxb@204s.com