国外大型固体火箭发动机立式贮存老化研究状况
|
摘要
固体火箭发动机的老化是决定导弹可靠性的关键问题。固体火箭发动机结构失效,包括药柱裂纹或壳体-衬层-推进剂界面脱粘往往会造成灾难性的后果。针对影响长期储存固体火箭发动机性能的固体推进剂老化问题,首先研究了固体推进剂的老化机理,概括总结了固体推进剂老化期间影响推进剂性能下降的物理因素和化学因素。在此基础上,分析了在发动机服役寿命分析中对固体推进剂的老化趋势进行预测所必需的老化监测数据要求。重点阐述了民兵导弹发动机老化监视计划的发展和实施情况,总结了不同阶段老化监视计划的研究重点及采用的不同试验方法。最后对大型立式储存发动机在长期自重载荷作用下,因药柱的几何形状发生改变而导致的推进剂下沉现象进行了分析,并总结了国外针对推进剂下沉问题所开展的模拟仿真进展,以期对工程上固体导弹发动机的贮存和使用提供参考。
Aging of solid rocket motors is a key issue determining the operational reliability of missiles. Structural failure of solid rocket motor,involving grain cracking or case-liner-propellant de-bonding,can occur with catastrophic results. Aiming at solid propellant aging issues,the aging mechanism of solid propellant was discussed,then some physical-chemical factors influencing propellant degradation during aging were summarized. On this basis,aging surveillance data required for assessing rocket motor service life were proposed. Secondly the paper focuses on the development of Minuteman propulsion surveillance program,analyzing the research emphasis and different test methods at different research period. Finally the simulation on propellant slump of large solid rocket motors during vertical storage condition was analyzed to provide reference for storage and operation of large solid rocket motor in engineering application.
Aging of solid rocket motors is a key issue determining the operational reliability of missiles. Structural failure of solid rocket motor,involving grain cracking or case-liner-propellant de-bonding,can occur with catastrophic results. Aiming at solid propellant aging issues,the aging mechanism of solid propellant was discussed,then some physical-chemical factors influencing propellant degradation during aging were summarized. On this basis,aging surveillance data required for assessing rocket motor service life were proposed. Secondly the paper focuses on the development of Minuteman propulsion surveillance program,analyzing the research emphasis and different test methods at different research period. Finally the simulation on propellant slump of large solid rocket motors during vertical storage condition was analyzed to provide reference for storage and operation of large solid rocket motor in engineering application.
引文
[1]J Edmund Fitzgerald,William L Hufferd.Handbook for the engineering structural analysis of solid propellants[R].AD887478.
[2]Eugene L Larson.A review of the Minuteman propulsion surveillance program for assessing rocket motor service life[R].AD467048.
[3]Hubner C,Geibler E,Elsner P.The Importance of micromechanical phenomena in energetic material[J].Propellants,Explosives,Pyrotechnics,1999,24(3):119-125.
[4]Kelley F N,Trout J L.Elements of solid rocket service life prediction[R].AIAA 72-1085.
[5]John L Myers,Edwin L Moon,Lemuel R Allen.Bibliography of solid rocket component aging[R].AD372032.
[6]Veit P V,Landuk L G,Simpson J V,et al.Evolution of an aging program Minuteman stage II solid rocket motor[R].ADA240864.
[7]Eugene L Larson,The minuteman propulsion surveillance program for assessing rocket motor service life[R].AD467048.
[8]Koford R E.Minuteman stageⅢmaterials and components surveillance program[R].ADA015429.
[9]Dennis F Malik.Storage reliability of missile materiel program,solid Propellant rocket motor[R].ADA026105.
[10]John A Thomson.Minuteman stage I motor reliability improvement program surveillance[R].ADA030640.
[11]Eugene F Lund.Minuteman long range service life analysis overview[R].AIAA 76-716.
[12]Bennett S J.LRSLA MinutemanⅢstageⅠmaterial characterization program and results[R].AIAA 76-718.
[13]Anderson G P.Minuteman stageⅠovertest results[R].AIAA 76-719.
[14]Ralph Davis.Minuteman III-surveillance semiannual report[R].ADA164840.
[15]Aerojet Strategic Propulsion Company.Aging and surveillance program MinutemanⅡ/Ⅲstage II program progress[R].ADA168269.
[16]Veit P W.Evolution of an aging program Minuteman stageⅡsolid rocket motor[R].AIAA 88-3328.
[17]Gregory Ruderman.Health management issues and strategy for air force missiles[R].ADA446283.
[18]Greg Ruderman,Eric Weber,Andrew Sincock.Health management and service life for air force missiles[R].ADA554598.
[19]James Fillerup,Robert Pritchard.Service life prediction technology program[R].ADA397950.
[20]Giuseppe S Tussiwand,Victor Saouma,Robert Terzenbach.Fracture mechanics of composite solid rocket propellant grains[J].Journal of Propulsion and Power,2009,25(1):60-73.
[21]Williams M L.The structural analysis of viscoelastic materials[R].AIAA 63-284.
[22]Aravas N,Xu F,Sofronis P,et al.Constitutive response and damage in solid propellants[R].AIAA 2005-4348.
[23]Namazifard A,Hjelmstad K,Sofronis P,et al.Simulations of propellant slumping in the Titan IV SRMU using constitutive models with damage evolution[R].AIAA 2005-3994.
[24]Fiedler R,Namazifard A,Campbell M,et al.Detailed simulations of propellant slumping in the Titan-IV SRMU PQM-1[R].AIAA 2006-4592.
[25]Sami Kilic,Arif Karabeyoglu,Jose Stevens,et al.Modeling the slump characteristics of the hydrocarbon-based hybrid rocket fuels[R].AIAA 2003-4461.
[2]Eugene L Larson.A review of the Minuteman propulsion surveillance program for assessing rocket motor service life[R].AD467048.
[3]Hubner C,Geibler E,Elsner P.The Importance of micromechanical phenomena in energetic material[J].Propellants,Explosives,Pyrotechnics,1999,24(3):119-125.
[4]Kelley F N,Trout J L.Elements of solid rocket service life prediction[R].AIAA 72-1085.
[5]John L Myers,Edwin L Moon,Lemuel R Allen.Bibliography of solid rocket component aging[R].AD372032.
[6]Veit P V,Landuk L G,Simpson J V,et al.Evolution of an aging program Minuteman stage II solid rocket motor[R].ADA240864.
[7]Eugene L Larson,The minuteman propulsion surveillance program for assessing rocket motor service life[R].AD467048.
[8]Koford R E.Minuteman stageⅢmaterials and components surveillance program[R].ADA015429.
[9]Dennis F Malik.Storage reliability of missile materiel program,solid Propellant rocket motor[R].ADA026105.
[10]John A Thomson.Minuteman stage I motor reliability improvement program surveillance[R].ADA030640.
[11]Eugene F Lund.Minuteman long range service life analysis overview[R].AIAA 76-716.
[12]Bennett S J.LRSLA MinutemanⅢstageⅠmaterial characterization program and results[R].AIAA 76-718.
[13]Anderson G P.Minuteman stageⅠovertest results[R].AIAA 76-719.
[14]Ralph Davis.Minuteman III-surveillance semiannual report[R].ADA164840.
[15]Aerojet Strategic Propulsion Company.Aging and surveillance program MinutemanⅡ/Ⅲstage II program progress[R].ADA168269.
[16]Veit P W.Evolution of an aging program Minuteman stageⅡsolid rocket motor[R].AIAA 88-3328.
[17]Gregory Ruderman.Health management issues and strategy for air force missiles[R].ADA446283.
[18]Greg Ruderman,Eric Weber,Andrew Sincock.Health management and service life for air force missiles[R].ADA554598.
[19]James Fillerup,Robert Pritchard.Service life prediction technology program[R].ADA397950.
[20]Giuseppe S Tussiwand,Victor Saouma,Robert Terzenbach.Fracture mechanics of composite solid rocket propellant grains[J].Journal of Propulsion and Power,2009,25(1):60-73.
[21]Williams M L.The structural analysis of viscoelastic materials[R].AIAA 63-284.
[22]Aravas N,Xu F,Sofronis P,et al.Constitutive response and damage in solid propellants[R].AIAA 2005-4348.
[23]Namazifard A,Hjelmstad K,Sofronis P,et al.Simulations of propellant slumping in the Titan IV SRMU using constitutive models with damage evolution[R].AIAA 2005-3994.
[24]Fiedler R,Namazifard A,Campbell M,et al.Detailed simulations of propellant slumping in the Titan-IV SRMU PQM-1[R].AIAA 2006-4592.
[25]Sami Kilic,Arif Karabeyoglu,Jose Stevens,et al.Modeling the slump characteristics of the hydrocarbon-based hybrid rocket fuels[R].AIAA 2003-4461.