反导末端拦截系统战斗部技术研究
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摘要
现代战争中,采用超低空方式突防的精确制导武器特别是战术巡航导弹的威胁日趋严重,对导弹的防御特别是高价值目标在未来战争中的生存问题已成为人们广为关注的热点之一。为了在未来战争中夺取反空袭作战的胜利,本文提出了一种用于要地防护的预设型反导末端拦截系统,并对其拦截弹的战斗部系统进行了细致的研究。
为了更有效地实现对超低空隐蔽入侵目标的毁伤,达到毁伤目标的多样性与毁伤目标的可靠性,在现有技术和理论研究基础上,设计了拦截弹的战斗部系统,系统采用周向均布多层小直径多爆炸成型弹丸爆炸形成的高速破片攻击进入弹道末端的空中目标,同时并辅以爆破战斗部技术。设计过程中,采用理论和经验分析初步设计和试验研究优化设计等多种手段相结合的综合方法,对小口径爆炸成型弹丸进行了科学合理的设计。侵彻钢板威力实验表明,小口径爆炸成型弹丸的设计能够满足战斗部末端反导作战的性能要求。因时间问题,战斗部整体外场静爆实验还没有进行,有待进一步实验。
对所设计战斗部的毁伤元进行了描述,建立了该战斗部的破片场数学模型,对战斗部的毁伤能力进行了相关理论计算,计算结果表明,所设计的拦截弹战斗部能够满足末端反导的性能要求。
In modern war,more and more precise control and guide weapns,especially cruise missile,have been used on many missions.so missile defence, particularly protecting the high-value objects against attack, becomes winning increasing attention.This paper devises a predefined antimissile terminal defence system used to protecting high-value objects to win the future anti-aircraft battle,and then designs its warhead in detail.
In order to dynamite the rival target that make an assault in low height efficiently, based on the analysis of the exsting technology and theory, the warhead system of the anti-missile is designed.The system has some layers of small caliber explosively formed projictile,after explosived,it formed many EFP to hit aircrafts,also it has capability of explosive warhead.In designing,we make use of synthetical method that includes theory analysis and experimental research,design appropriate small caliber explosively formed projictile. Experiments indicate the design of small caliber explosively formed projictile can fulfil the capability demand of terminal defence.Because of time short,the warhesd static experiments are not carried out,need to be done next time.
In paper,depict kill elements that the warhead formed,constitute warhead fregment athematical-physical model,then calculate its kill capability in theory,the results show that the warhead system designed in this paper is competent for antimissile terminal defence task.
为了更有效地实现对超低空隐蔽入侵目标的毁伤,达到毁伤目标的多样性与毁伤目标的可靠性,在现有技术和理论研究基础上,设计了拦截弹的战斗部系统,系统采用周向均布多层小直径多爆炸成型弹丸爆炸形成的高速破片攻击进入弹道末端的空中目标,同时并辅以爆破战斗部技术。设计过程中,采用理论和经验分析初步设计和试验研究优化设计等多种手段相结合的综合方法,对小口径爆炸成型弹丸进行了科学合理的设计。侵彻钢板威力实验表明,小口径爆炸成型弹丸的设计能够满足战斗部末端反导作战的性能要求。因时间问题,战斗部整体外场静爆实验还没有进行,有待进一步实验。
对所设计战斗部的毁伤元进行了描述,建立了该战斗部的破片场数学模型,对战斗部的毁伤能力进行了相关理论计算,计算结果表明,所设计的拦截弹战斗部能够满足末端反导的性能要求。
In modern war,more and more precise control and guide weapns,especially cruise missile,have been used on many missions.so missile defence, particularly protecting the high-value objects against attack, becomes winning increasing attention.This paper devises a predefined antimissile terminal defence system used to protecting high-value objects to win the future anti-aircraft battle,and then designs its warhead in detail.
In order to dynamite the rival target that make an assault in low height efficiently, based on the analysis of the exsting technology and theory, the warhead system of the anti-missile is designed.The system has some layers of small caliber explosively formed projictile,after explosived,it formed many EFP to hit aircrafts,also it has capability of explosive warhead.In designing,we make use of synthetical method that includes theory analysis and experimental research,design appropriate small caliber explosively formed projictile. Experiments indicate the design of small caliber explosively formed projictile can fulfil the capability demand of terminal defence.Because of time short,the warhesd static experiments are not carried out,need to be done next time.
In paper,depict kill elements that the warhead formed,constitute warhead fregment athematical-physical model,then calculate its kill capability in theory,the results show that the warhead system designed in this paper is competent for antimissile terminal defence task.
引文
[1]赵江,徐世录.反巡航导弹的现状与发展趋势[J].飞航导弹,2005,5:52-58.
[2]谢建华.近程防空系统在防空体系中的作用和意义[J].军事技术,1996.
[3]黎春林,冯顺山.超近程反导武器系统探讨[J].现代防御技术,2003,31(1):12-14.
[4]吕久明,罗景青.巡航导弹强弱点分析及防御方法[J].火力与指挥控制,2006,31(2):1-4.
[5]刘治德,等.21世纪的精确制导武器技术[J].解放军报.
[6]姜春兰.弹药学[M].北京:中国兵器工业出版社,2000年5月.
[7]李补莲.新兵器空-地对抗形势下防空系统的发展[J].火力与指挥控制,2005,30(增刊):7-10.
[8]李向东.蔡振华.防空高炮弹药[J].现代兵器,2004,2.
[9]于骐.弹药学[M].北京:国防工业出版社,1987年12月.
[10]郭福清译.拦截导弹的AHEAD炮弹[J].飞航导弹,1994,5:10-11.
[11]李静海.反舰导弹与防空导弹战斗部的发展研究[J].战术导弹技术,2001,1:17-22.
[12]赵晓尧,刘天生.提高战斗部威力的几种途径[J] .产品开发与设计,2005,4:33-35.
[13]陈兢.未来防空反导的杀手锏[J].现代军事,2006,8:60-62.
[14]中国航天工业总公司《世界导弹大全》修订委员会.世界导弹大全[M].北京:军事科学出版社,1998.
[15] RePort of the Defense Seienee Board Summer Study on Cruise Missile Defonse,Undersecretary of Defense for Acquisition&Teehnology,Washington,DC,Jan.1995,P.14.
[16]杨少宇,秦峰.防空高炮现状与发展趋势分析[J].四川兵工学报.2003(6):3-6.
[17] M.Held.Fragmentation Warhead,Tactical missile Warhead.AIAA,1993.
[18]刘淑英,邵元培,计世藩.用战术激光武器反巡航导弹[J].现代防御技术.2001,5.
[19]倪树新.光电技术用于反巡航导弹的探讨[J].激光与红外.1999,5.
[20]王晓鸣.反直升机智能雷武器系统总体及关键技术研究[D].南京理工大学博士学位论文(2002).
[21]蒋浩征,周兰庭,蔡汉文.火箭战斗部设计原理[M].北京:国防工业出版社,1982.
[22] Fong R . Multile explosively formed Penetrator warhead teehnologies.19th international symposium on ballisties.the seeond volume,2001.563~568.
[23]姜辉,郭美芳.爆炸成型弹丸译文集[M].北京:兵器工业总公司,2006,6.
[24]任辉启,杨仁华,吴祥云.高效毁伤弹药工程破坏效应研究.GF报告,2005.
[25]爆炸及其作用[M].北京:国防工业出版社,1979.
[26]叶序双.爆炸作用基础[M].南京:解放军理工大学工程兵工程学院,2001.
[27]隋树元,王树山.终点效应学[M].北京:国防工业出版社,2000.
[28] Chou P C、Flis W J.Recent development in shaped charge technolog. Propellnats、Explosives,Pyrotechnies,11,1986
[29]张国伟.终点效应及其应用[M].北京:国防工业出版社,2006.
[30]何顺录.自锻破片技术的发展[M].北京:北京理工大学出版社,1996.
[31] W.P.Walters,J.A.Zukas.Fundamentals of Shaped Charge.Proc. of the 12th.International symposium on ballastics.1990
[32] Jan L.M.J.Van Bree,Willem Duvalois.Effects of Desigh Parameters of an EFP Charge on Projectile Stability.Proc. of the16th. International Symposium on Ballastics.1996
[33]陶钢,朱鹤荣,石连捷.爆炸成型弹丸药型罩结构分析[J].弹道学报,1995,7(3).
[34]何顺录,李录荫.自锻破片技术的研究现状和发展.破甲文集(六).南京:中国兵工学会弹药分会,1987.
[35]彭庆明.自锻破片战斗部设计方法的讨论.第四届破甲会议文集.陕西:中国兵工学会弹药分会,1984.
[36]陶钢,朱鹤荣,石连捷.关于爆炸成型弹丸(EFP)的研究[J].1995,7(3).
[37]林溪石.反直升机地雷原理与实践[M].北京:兵器工业出版社,2006.
[38]杨仁华.聚能装药对岩土介质的侵彻研究[D],长沙:国防科学技术大学博士学位论文,2003.
[39]崔秉贵.弹药战斗部工程设计[M].北京理工大学出版社,1995.
[40]魏惠之,朱鹤松,汪东晖,等.弹丸设计理论[M].北京:国防工业出版社,1985.
[41]庄志洪,刘剑锋等.引战配合效率分析[J].兵工学报,2001,22(1).
[42]王儒策,赵国志.弹丸终点效应[M].南京:南京理工大学出版社,1991.
[43]赵国志,张运法,沈培辉,李向东编译.常规战斗部系统工程设计[M].南京:南京理工大学出版社,2000.
[44]北京工业学院八系.爆炸及其作用[M].北京:国防工业出版社.1979.
[45] Renders-pehrson G.An Improved Equation For Calculating Fragment Perferction Angles[P].Proc.Of the 2nd Int.Symp.On Ballistics.1976.
[46]李必红. EFP装药技术在破碎混凝土桩砦中的应用研究[D],中南大学硕士学位论文,2004.
[47]戴端辉,黄超会.预制破片弹杀伤面积的计算[J].兵工学报,1998,19(4).
[48]赵文宣.终点弹道学[M].北京:兵器工业出版社,1985.
[49]庄志洪,路建伟等.破片速度衰减对命中目标部位的影响[J].弹道学报.1999,11(2).
[50] Manfted Held, Explosivstoff, Vol. 16, No. 5, 1968
[51] Manfred Held, Initiation phenomena with shaped charge jets, Proc. of 9th(int.) symp.on detonation, 1981.
[52] RichardM L.Conventional warhead systems physics and engineering design[M] Virginia:American lnstitute of Aeronautics and A stronautics, 1nc, 1998: 502-504.
[2]谢建华.近程防空系统在防空体系中的作用和意义[J].军事技术,1996.
[3]黎春林,冯顺山.超近程反导武器系统探讨[J].现代防御技术,2003,31(1):12-14.
[4]吕久明,罗景青.巡航导弹强弱点分析及防御方法[J].火力与指挥控制,2006,31(2):1-4.
[5]刘治德,等.21世纪的精确制导武器技术[J].解放军报.
[6]姜春兰.弹药学[M].北京:中国兵器工业出版社,2000年5月.
[7]李补莲.新兵器空-地对抗形势下防空系统的发展[J].火力与指挥控制,2005,30(增刊):7-10.
[8]李向东.蔡振华.防空高炮弹药[J].现代兵器,2004,2.
[9]于骐.弹药学[M].北京:国防工业出版社,1987年12月.
[10]郭福清译.拦截导弹的AHEAD炮弹[J].飞航导弹,1994,5:10-11.
[11]李静海.反舰导弹与防空导弹战斗部的发展研究[J].战术导弹技术,2001,1:17-22.
[12]赵晓尧,刘天生.提高战斗部威力的几种途径[J] .产品开发与设计,2005,4:33-35.
[13]陈兢.未来防空反导的杀手锏[J].现代军事,2006,8:60-62.
[14]中国航天工业总公司《世界导弹大全》修订委员会.世界导弹大全[M].北京:军事科学出版社,1998.
[15] RePort of the Defense Seienee Board Summer Study on Cruise Missile Defonse,Undersecretary of Defense for Acquisition&Teehnology,Washington,DC,Jan.1995,P.14.
[16]杨少宇,秦峰.防空高炮现状与发展趋势分析[J].四川兵工学报.2003(6):3-6.
[17] M.Held.Fragmentation Warhead,Tactical missile Warhead.AIAA,1993.
[18]刘淑英,邵元培,计世藩.用战术激光武器反巡航导弹[J].现代防御技术.2001,5.
[19]倪树新.光电技术用于反巡航导弹的探讨[J].激光与红外.1999,5.
[20]王晓鸣.反直升机智能雷武器系统总体及关键技术研究[D].南京理工大学博士学位论文(2002).
[21]蒋浩征,周兰庭,蔡汉文.火箭战斗部设计原理[M].北京:国防工业出版社,1982.
[22] Fong R . Multile explosively formed Penetrator warhead teehnologies.19th international symposium on ballisties.the seeond volume,2001.563~568.
[23]姜辉,郭美芳.爆炸成型弹丸译文集[M].北京:兵器工业总公司,2006,6.
[24]任辉启,杨仁华,吴祥云.高效毁伤弹药工程破坏效应研究.GF报告,2005.
[25]爆炸及其作用[M].北京:国防工业出版社,1979.
[26]叶序双.爆炸作用基础[M].南京:解放军理工大学工程兵工程学院,2001.
[27]隋树元,王树山.终点效应学[M].北京:国防工业出版社,2000.
[28] Chou P C、Flis W J.Recent development in shaped charge technolog. Propellnats、Explosives,Pyrotechnies,11,1986
[29]张国伟.终点效应及其应用[M].北京:国防工业出版社,2006.
[30]何顺录.自锻破片技术的发展[M].北京:北京理工大学出版社,1996.
[31] W.P.Walters,J.A.Zukas.Fundamentals of Shaped Charge.Proc. of the 12th.International symposium on ballastics.1990
[32] Jan L.M.J.Van Bree,Willem Duvalois.Effects of Desigh Parameters of an EFP Charge on Projectile Stability.Proc. of the16th. International Symposium on Ballastics.1996
[33]陶钢,朱鹤荣,石连捷.爆炸成型弹丸药型罩结构分析[J].弹道学报,1995,7(3).
[34]何顺录,李录荫.自锻破片技术的研究现状和发展.破甲文集(六).南京:中国兵工学会弹药分会,1987.
[35]彭庆明.自锻破片战斗部设计方法的讨论.第四届破甲会议文集.陕西:中国兵工学会弹药分会,1984.
[36]陶钢,朱鹤荣,石连捷.关于爆炸成型弹丸(EFP)的研究[J].1995,7(3).
[37]林溪石.反直升机地雷原理与实践[M].北京:兵器工业出版社,2006.
[38]杨仁华.聚能装药对岩土介质的侵彻研究[D],长沙:国防科学技术大学博士学位论文,2003.
[39]崔秉贵.弹药战斗部工程设计[M].北京理工大学出版社,1995.
[40]魏惠之,朱鹤松,汪东晖,等.弹丸设计理论[M].北京:国防工业出版社,1985.
[41]庄志洪,刘剑锋等.引战配合效率分析[J].兵工学报,2001,22(1).
[42]王儒策,赵国志.弹丸终点效应[M].南京:南京理工大学出版社,1991.
[43]赵国志,张运法,沈培辉,李向东编译.常规战斗部系统工程设计[M].南京:南京理工大学出版社,2000.
[44]北京工业学院八系.爆炸及其作用[M].北京:国防工业出版社.1979.
[45] Renders-pehrson G.An Improved Equation For Calculating Fragment Perferction Angles[P].Proc.Of the 2nd Int.Symp.On Ballistics.1976.
[46]李必红. EFP装药技术在破碎混凝土桩砦中的应用研究[D],中南大学硕士学位论文,2004.
[47]戴端辉,黄超会.预制破片弹杀伤面积的计算[J].兵工学报,1998,19(4).
[48]赵文宣.终点弹道学[M].北京:兵器工业出版社,1985.
[49]庄志洪,路建伟等.破片速度衰减对命中目标部位的影响[J].弹道学报.1999,11(2).
[50] Manfted Held, Explosivstoff, Vol. 16, No. 5, 1968
[51] Manfred Held, Initiation phenomena with shaped charge jets, Proc. of 9th(int.) symp.on detonation, 1981.
[52] RichardM L.Conventional warhead systems physics and engineering design[M] Virginia:American lnstitute of Aeronautics and A stronautics, 1nc, 1998: 502-504.