[1]解红雨,周伟勇,吴勋,等.固体火箭发动机寿命预估方法研究进展[J].固体火箭技术,2019,42(03):377-383.
 XIE Hongyu,ZHOU Weiyong,WU Xun,et al.Research progress on the service life prediction method for the solid rocket motor[J].Journal of Solid Rocket Technology,2019,42(03):377-383.
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固体火箭发动机寿命预估方法研究进展

参考文献/References:

[1]孟涛,张仕念,易当祥,等.导弹贮存延寿技术概论[M].北京:中国宇航出版社,2013.MENG Tao,ZHANG Shinian,YI Dangxiang,et al.Storage and life extension general technology for the missile[M].Beijing: China Aerospace Press,2013.[2]王铮.固体火箭发动机使用寿命的预估和“延寿”[J].固体火箭技术,1999,22(1):23-29.WANG Zheng.Service life prediction and “prolong” for the solid rocket motor[J].Journal of Solid Rocket Technology,1999,22(1):23-29.[3]董可海,邢耀国.固体火箭发动机寿命预估研究的发展和展望[J].固体火箭技术,2001,24(3):30-33.DONG Kehai,XING Yaoguo.Progress and prospect of life prediction technique for solid rocket motor[J].Journal of Solid Rocket Technology,2001,24(3):30-33. [4]Hiltmar Schubert.Service life determination of rocket motor by comprehensive property analysis of propellant grains[R].AD-A330303.[5]Russakov Loren S,Whalley Lan A.Accelerated aging testing of energetic components:A current assessment of methodology[R].AIAA 2000-3646.[6]徐丹丹,闫大庆.国外固体火箭发动机整机试验技术现状[J].飞航导弹,2017(11):85-91.XU Dandan,YAN Daqing.Oversea situation of whole solid rocket motor test technology[J].Winged Missiles Journal,2017(11):85-91.[7]吴力力,丁玉奎,甄建伟.国外弹药延寿研究现状[J].飞航导弹,2018(3):74-78.WU Lili,DING Yukui,ZHEN Jianwei.Oversea situation of ammunition life extension[J].Winged Missiles Journal,2018(3):74-78. [8]周东谟.定应变下HTPB推进剂老化机理及发动机寿命预估研究[D]北京:北京理工大学,2016.ZHOU Dongmo.Aging mechanism of HTPB propellant under constant strain and life prediction of solid rocket motors[D].Beijing: Beijing Institute of Technology,2016.[9]George D,Blair M.Overview of the integrated high payoff rocket propulsion technology (IHPRPT) program[R].AD-411290,2003.[10]LIU C T.Fracture mechanics and service life prediction research[R]A-410141,2003.[11]袁端才,唐国金,李海阳,等.基于加速老化与三维粘弹性有限元分析的固体导弹发动机寿命预估[J].兵工学报.2006,27(4):685-689.YUAN Duancai,TANG Guojin,LI Haiyang,et al.Three-dimension viscoelastic analysis and accelerated aging approach to predict the service life of solid missile motor[J].Acta Armamentarii,2006,27(4):685-689.[12]Herrmaun C R.An application of the “requirement vs capability” analysis to estimating design reliability of solid rocket motor[R].NASA N70-22698.[13]Bills K W,et al.The chemical kinetic approach to service life predication of propellant system[R].AIAA 79-243.[14]Heller R A,Kamat MP,Singht MP.Probability of solid propellant motor failure due to environmental temperatures[J].JSR,1979,16(3):140-146.[15]周堃,胡滨,王津梅,等.阿伦尼乌斯公式在阿伦尼乌斯公式在弹箭贮存寿命评估中的应用[J].装备环境工程.2011,8(4):1-5.ZHOU Kun,HU Bin,WANG Jinmei,et al.application of Arrhenius equation in storage life evaluation of ammunition[J].Equipment Environmental Engineering,2011,8(4):1-5.[16]韩龙,刘梅,高波,等.固体发动机药柱完整性失效的判据[J].固体火箭技术,2018,41(4):424-427.HAN Long,LIU Mei,GAO Bo,et al.Failure criterion of solid motors at ignition pressurization loading[J].Journal of Solid Rocket Technology,2018,41(4):424-427.[17]刘子如.火炸药老化失效模式及机理[J].火炸药学报,2018,41(5):425-433.LIU Ziru.Failure modes and failure mechanisms for aged propellants and explosives[J].Chinese Journal of Explosives & Propellants,2018,41(5): 425-433.[18]王卫国,朱觅.空空导弹固体火箭发动机贮存寿命探讨[J].四川兵工学报,2007(6):17-19.WANG Weiguo,ZHU Mi.Investigate the storage life for the air to air solid missile motor[J].Journal of Sichuan Ordnance.2007(6):17-19.[19]邢耀国,董可海,沈伟,等.固体火箭发动机使用工程[M].北京:国防工业出版社,2010.XING Yaoguo,DONG Kehai,SHEN Wei,et al.Using project for solid rocket motor[M].Beijing: Natianal Defense Industry Press,2010.[20]Chaitanya S S,Mahendra J P,Madhav V P.Accelerated aging and life time prediction analysis of polymer composites: a new approach for a realistic prediction using cumulative damage theory [J].Polymer Testing,1994,13:295-322.[21]Bills K W.Solid propellant cumulative damage program-final report[R].AFRPL-TR-68-131.[22]唐国金,申志彬,田四朋,等.固体火箭发动机药柱概率贮存寿命预估[J].兵工学报.2012,33(3):301-306.TANG Guojin,SHEN Zhibin,TIAN Sipeng.Probabilistic storage life prediction of solid rocket motor grain[J].Acta Armamentarii,2012,33(3):301-306.[23]刘文亮,衡淑云,岳璞,等.NEPE推进剂贮存寿命预估方法的比较[J].化学分析计量,2011,20(s):77-81.LIU Wenliang,HENG Shuyun,YUE Pu,et al.Prediction method comparision for NEPE propellant storage life[J].Chemical Analysis and Meterage,2011,20(s):77-81.[24]职世君,张建伟,张泽远.复合固体推进剂细观损伤形貌数值模拟[J].固体火箭技术,2015,38(2):239-244.ZHI Shijun,ZHANG Jianwei,ZHANG Zeyuan.Numerical simulation of mesoscopic damage morphology of composite solid propellants[J].Journal of Solid Rocket Technology,2015,38(2):239-244.[25]韩龙.复合固体推进剂细观损伤机理及本构模研究[D].南京:南京理工大学,2016.HAN long.Research on the mesoscopic damage mechanism and nonlinear viscoelastic constitutive model of composite propellant[D].Nanjing: Nanjing University of Science & Technology,2016,11. [26]周献刚,杨明.HTPB 推进剂粘接界面细观蠕变试验及本构模型研究[J].计算机与数字工程,2018,46(9):1921-1926.ZHOU Xiangang,YANG Ming.Study on meso-creep test and constitutive model of HTPB propellant adhesive interface[J]Computer & Digital Engineering,2018,46(9):1921-1926.[27]郭洪涛,曹付齐.界面粘接结构贮存过程的脱粘分析[J].粘接,2013(6):47-49.GUO Hongtao,CAO Fuqi.Debond analysis of interface bonding strucutre during storage[J].Adhesion,2013(6):47-49.[28]毛丹,马浩然,杨根,等.衬层/推进剂界面粘接优劣的判定和时空特征[J].固体火箭技术,2016,39(6):779-783.MAO dan,MA Haoran,YANG Gen,et al.Judgment method and timespace characteristic of the interface between liner and propellant[J].Journal of Solid Rocket Technology,2016,39(6):779-783.[29]吴丰军,彭松,池旭辉.NEPE推进剂/衬层粘接界面细观力学性能/结构研究.[J].固体火箭技术,2010,33(1):81-85.WU Fengjun,PENG Song,CHI Xuhui.Study on microcosmic mechanics performance/structure of NEPE propellant/liner bonded interface[J].Journal of Solid Rocket Technology,2010,33(1):81-85.[30]张守诚,屈文忠,肖黎.固体发动机界面结构试件脱粘健康监测研究.[J].固体火箭技术,2017,40(3):319-324.ZHANG Shoucheng,QU Wenzhong,XIAO Li.Research on health monitoring of insulator/propellant interface debonding in solid rocket motor[J].Journal of Solid Rocket Technology,2017,40(3):319-324.[31]李高春,姜爱民,黄卫东,等.固体火箭发动机粘接界面变形破坏的细观试验与数值模拟[J]火炸药学报,2018,41(3):314-318.LI Gaochun,JIANG Aimin,HUANG Weidong,et al.Meso-experiment and numerical simulation of deformation and failure adhesive interface for solid rocket motor[J].Chinese Journal of Explosives & Propellants,2018,41(3): 314-318.[32]高鸣,任海峰.固体仪器发动机健康监测技术评述与研究[J].固体火箭技术,2013,36(2):278-284.GAO Ming,REN Haifeng.Review and research on health monitoring of solid rocket motors based on instrumented motor[J].Journal of Solid Rocket Technology,2013,36(2):278-284.[33]吴勋,任宁莉,冯翔,等.固体发动机典型环境载荷分析.装备环境工程,2010,7(6):103-106.WU Xun,REN Ningli,FENG Xiang,et al.Analysis of typical environmental load of solid rocket motor[J].Equipment Environmental Engineering,2010,7(6):103-106.[34]张波,董可海,张春龙,等.固体火箭发动机健康监测系统及其关键技术研究[J].舰船电子工程,2013,33(10):88-91.ZHANG Bo,DONG Kehai,ZHANG Chunlong,et al.Solid rocket engine health monitoring system and its key technology research[J].Ship Electronic Engineering,2013,33(10):88-91[35]陈海建,石伟峰.导弹固体火箭发动机贮存寿命预测方法研究[J].现代防御技术,2016,44(3):148-154.CHEN Haijian,SHI Weifeng.Method of predicting storage life of missile solid rocket motor[J].Modern Defence Technology,2016 ,44(3):148-154.[36]杜永强,郑坚,彭威,等.HTPB推进剂贮存老化建模及寿命预估研究综述[J].化工进展,2016,35(Z2):219-225.DU Yongqiang,ZHENG Jian,PENG Wei,et al.Review of the research of aging modeling and life prediction for HTPB propellant[J].Chemical Industry and Engineering Progress,2016,35(Z2):219-225.[37]高江,于晓梅,宋其其.固体推进剂药柱综合寿命评估方法研究[J].战术导弹技术,2011(3):43-47.GAO Jiang,YU Xiaomei,SONG Qiqi.Combined life evaluation method for solid propellant grain[J].Tactical Missile Technology,2011(3):43-47

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更新日期/Last Update: 2019-07-11
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