战术导弹固体发动机低易损性改进对人员及财产具有重要的意义,近年来成为一种重要发展方向。欧美等国家经过近50年的发展,已经形成了较为完备的试验标准和评估方法,积累了大量的低易损改进经验。文中通过对国外低易损试验标准及评估的发展过程、固体发动机低易损性改进进展以及低易损试验进行分析,为国内战术导弹固体发动机低易损性改进提供了参考。
The low vulnerability improvement of tactical missile solid motor is of great significance to personnel and property. And it has become an important development direction in recent years. After 50 years evolution, Europe and the United States have formed relatively complete test standards and assessment methods, and accumulated a lot of experience in the improvement of low vulnerability. This article provides a reference for the low vulnerability improvement of domestic tactical missile solid engine, by analyzing the development process of the foreign low vulnerability test standard and criterion, progress in low vulnerability improvement of solid rocket motor and low vulnerability test.
[an error occurred while processing this directive]
[1] SWANSON R L. Approach to IM policy:defining the need[R].[S.l.]:Munitions Safety Information Analysis Center,2015.
[2] SWIERK T. IM testing and assessments:STO-EN-AVT-214[R].Virginia:Naval Surface Warfare Center,2015.
[3] Department of Defense:Hazard assessment tests for non-nuclear munitions:MIL-STD-2105D[S].[S.l.:s.n.],2013.
[4] NATO Standardization Agency. Policy for introduction and assessment of insensitive munitions (IM):NATO STANAG 4439-2010[S].[S.l.]:NATO,2010.
[5] MOORE T L. Solid rocket development at Allegany Ballistics Laboratory:AIAA 99-2931[R].Redston:AIAA Inc.,1999.
[6] KESNER C,WINEBRENNER J,HARRIS R. Using safe, proven fuze technology for rocket motor ISDs:AIAA 2005-4500[R].Redston:AIAA Inc.,2005.
[7] POWELL I J.Insensitive munitions:design principles and technology developments[J].Propellants, Explosives, Pyrotechnics,2016,41(3):409-413.
[8] MOULARD H,DELCLOS A,KURY J. The effect of RDX particle size on the shock sensitivity of cast PBX formulations[C]//Proceedings of the Beijing International Symposium on Pyrotechnics and Explosives (ISPE).[S.l.:s.n.],1987:903-913.
[9] DAVENAS A.Development of modern solid propellants[J].Journal of Propulsion & Power,2003,19(6):1108-1128 .
[10] VERBERNE O,SKRIVERVIK O. History of the Nammo Raufoss rocket motor division:AIAA 2005-3806[R].Redston:AIAA Inc.,2005.
[11] GRAHAM K J. Insensitive munitions:Industry problems and solutions:STO-EN-AVT-214[R].[S.l.]:NATO,2015.
[12] FISHER M J,MOORE T L. Composite motor cases for tactical missile propulsion systems:AIAA 2005-3611[R].Redston:AIAA Inc.,2005.
[13] FOSSUMSTUEN K,RAUDSANDMOEN G,HEIE I,et al. Design verification programme for an air-to-air type rocket motor with CFRP composite case and reduced smoke propellant:AIAA 93-2320[R].Redston:AIAA Inc.,1993.
[14] TENDEN S. Development of the Composite Rocket Motor Case for a Hypervelocity Demonstration Program:AIAA 2007-5791[R].Redston:AIAA Inc.,2007.
[15] FLOTTEN B C. Insensitive munitions technology transition program composite case captive carry qualification (C4Q) :final report[R].China Lake :Naval Air Warfare center Weapons Division,2005.
[16] JAMESON A. Insensitive munitions testing of a rocket motor suitable for future air-to-air missiles:AIAA 97-3129[R].Redston:AIAA Inc.,1997.
[17] AMOS R J. Structural testing of the bonded body for an insensitive munitions air-to-air missile:AIAA 97-3130[R].Redston:AIAA Inc.,1997.
[18] STRICKLAND A. Development of IM Brimstone rocket motor:an IM, minimum smoke, air-launched system[C]//Proceedings of 2015 Insensitive Munitions and Energetic Materials Technology Symposium.[S.l.:s.n.],2015:1-9.