Page 44 - 《含能材料》优秀论文(2019年)
P. 44

三 氢 化 铝 合 成 及 应 用 评 价 技 术 进 展                                                                     325

                Compositions:USP 3,785,890[P],1974.             [42] 刘晶如,辛伟,杨寅 . 含金属氢化物推进剂的能量特性计算研究
           [35] Matzek N E,Roehrs H C. Stabilization of Light Metal Hydride:  [J]. 火工品,2010(2):37-40.
                USP 3,857,922[P],1974.                               LIU Jing⁃ru,XIN Wei,YANG Yin. The Computational investi⁃
           [36] Petrie M A,Bottaro J C,Schmitt R J,et al. Preparation of Alu⁃  gation of energy characteristics of propellant containing metal
                minum Hydride Polymorphs, Particularly Stabilizedα⁃AlH 3 :  hydride[J]. Initiators & Pyrotechnics,2010(2):37-40.
                USP 628338B1[P],2001.                           [43] Shark S C,Sippel T R,Son S F,et al. Theoretical Performance
           [37] Petrie M A,Bottaro J C,Schmitt R J,et al. Stabilized Alumi⁃  Analysis of Metal Hydride Fuel Additives for Rocket Propellant
                num Hydride Polymorphs:USP 6617064B2[P],2003.        Applications[C]//47th AIAA/ASME/SAE/ASEE Joint Propulsion
           [38] 刘明星,三氢化铝的合成及稳定化技术研究[D]. 湖北:湖北航                       Conference & Exhibit,San Diego,California,August 2011.
                天化学技术研究所,2008.                                  [44] Bazyn T,Eyer R,Krier H. Combustion characteristics of alumi⁃
                LIU Ming⁃xing. Synthesis and Stabilization of Aluminum Hy⁃  num hydride at elevated pressure and temperature[J]. Journal
                dride[D]. Hubei:Hubei Institute of Aerospace Chemotechnol⁃  of propusion and power,2012,20(3):427-431.
                ogy,2008.                                       [45] Deluca L T,Rossettini L,Kappenstein C,et al. Ballistic char⁃
           [39] 李磊 . AlH 3 混合体系机械感度的相互作用机理研究[D]. 湖北:                 acterization of AlH 3 ⁃based propellants for solid and hybrid
                湖北航天化学技术研究所,2014.                                    rocket propulsion[C]//45th AIAA / ASME / SAE / ASEE Joint Pro⁃
                LI Lei. Study on the interaction of mechanical sensitivity of  pulsion Conference & Exhibit,Denver,Colorado,2009.
                AlH 3 mixed system[D]. Hubei:Hubei Institute of Aerospace  [46] Deluca L T,Galfetti L,Severini F. Physical and ballistic char⁃
                Chemotechnology,2014.                                acterization of AlH 3 ⁃based space propellants[J]. Aerospace Sci⁃
           [40] 张伟,刘运飞,谢五喜,等 . 热分析法研究 AlH 3 与固体推进剂组                  ence and Technology,2007,(1):18-25.
                分的相容性[J]. 火炸药学报,2015(1):41-46.                  [47] Flynn J P. Nitrocellulose propellant composition containing
                ZHANG Wei,LIU Yun⁃fei,XIE Wu⁃xi,et al. Study on compat⁃  aluminum hydride:USP 3844856[P],1975.
                ibility of AlH 3 with compositions of solid propellant by thermal  [48] Ermilov A S. Solid rocket fuel:RUP 2241693[P],2004.
                analysis methed[J]. Chinese Journal of Explosives &Propel⁃  [49] 徐星星,唐根,胡翔,等 . AlH 3 固体推进剂能量性能的理论研究
                lants,2015(1):41-46.                                [J]. 化学推进剂与高分子材料,2017,15(6):58-63.
                                                                     XU Xing⁃xing,TANG Gen,HU Xiang,et al. Theoretical re⁃
           [41] 王 艳 群 ,王 宝 山 ,李 伟 . 硝 化 甘 油 在 α⁃Al 2 O 3 (0001)和 γ⁃Al 2 O 3
                (110)表面吸附的理论计算[J]. 高等学校化学学报,2017,38                  search on energy performance of AlH 3 ⁃based solid propellant
                (8):1383-1389.                                      [J]. Chemical Propellants & Polymeric Materials,2017,15
                WANG Yan⁃qun,WANG Bao⁃shan,LI Wei. Theoretical inves⁃  (6):58-63.
                tigation on the adsorption of nitroglycerin on α⁃Al 2 O 3 (0001)  [50] Glumac N,Bazyn T,Eyer R,et al. The combustion character⁃
                and γ⁃Al 2 O 3 (110) surfaces[J]. Chemical Journal of Chinese  istics o f aluminum hydride under solid rocket motor condi⁃
                Universities,2017,38(8):1383-1389.                   tions[R]. Grafiche GSS,2004.



            Recent Progresses on Synthesis and Evaluation of AlH 3

            PANG Ai⁃min 1,2 ,ZHU Zhao⁃yang 1,2 ,XU Xing⁃xing 2
           (1. Science and Technology on Aerospace Chemical Power Laboratory,Xiangyang 441003,China;2. Hubei Institute of Aerospace Chemical Technology,
            Xiangyang 441003,China)
            Abstract:Aluminum hydride(AlH 3 )has high hydrogen content capacity(mass content>10%),low molecular weight of com⁃
            bustion products and relatively high thermal decomposition temperature. AlH 3 can significantly improve the energy level of solid
            propellants by partially replacing aluminum powder,so it is considered as a very important high⁃energy fuel. However,there is
            critical dependence of the solid propellant performances on the quality of AlH 3 crystals. The choice and optimization of prepara⁃
            tion method largely determines the quality and cost of the products. It has been shown that the unstable nature of AlH 3 could
            greatly affect the aging and storage performances. Moreover,the incompatibility between some components and AlH 3 decreases
            the safety of corresponding solid propellants. The problems mentioned above are the key technical issues and need to be solved
            before large⁃scale application of AlH 3 in solid propellant formulations. The advances in synthetic techniques for AlH 3 and its ap⁃
            plication in solid propellants over the world have been introduced in this review paper. The stabilizing strategies and post evalua⁃
            tion of AlH 3 in relevant research institutes are summarized as well,based on which the future research directions are proposed.
            The literature shows that the safety and quality control during scaling⁃up of AlH 3 can be solved by using ether synthetic method.
            The applicability of AlH 3 in solid propellant can be greatly improved by surface treatment,including coating of AlH 3 .
            Key words:Aluminum hydride;synthesis;solid propellants;high energy fuel;stability
            CLC number:TJ55;V512                       Document code:A                  DOI:10.11943/CJEM2019004
                                                                                                     (责编:张 琪)





            CHINESE JOURNAL OF ENERGETIC MATERIALS              含能材料                2019 年  第 27 卷  第 4 期 (317-325)
   39   40   41   42   43   44   45   46   47   48   49