期刊文献+

固体推进剂药柱的可靠性评估技术 被引量:4

Evaluation Methods of Solid Propellant Grain Reliability
下载PDF
导出
摘要 为满足目前固体发动机研制的可靠性需要,对固体推进剂药柱的结构可靠性因素、评估方法以及可靠性评估中药柱失效模式的研究情况等进行了评述。对过载试验的原则和实例以及药柱可靠性评估所涉及的3个研究领域(失效判据、结构分析方法和推进剂响应与失效性质)存在的关键问题及其研究状况进行了详细介绍。指出了固体药柱可靠性评估技术亟待解决的一些问题和发展方向。 In order to meet the demand of developing the evaluation methods for reliability of solid rocket motor, the current situation about structural reliability factors, evaluation methods and failure modes in reliability evaluation of solid propellant grain are reviewed. The overload test firing principles and examples, the existing problems and major pioneer studies in three research areas involved in grain reliability evaluation, namely failure criteria, structural analysis methods, as well as propellant response and failure properties, are discussed in detail. The problems faced are presented, and the development directions are pointed out.
出处 《火炸药学报》 EI CAS CSCD 2008年第1期68-71,共4页 Chinese Journal of Explosives & Propellants
关键词 固体推进剂 药柱 可靠性评估 失效模式 solid propellant grain reliability evaluation failure modes
  • 相关文献

参考文献9

  • 1Akpan U O,Dunbar T E,Franklin C W,et al.Probabilistic risk assessment of solid-propellant rocket motors[J].Journal of Spacecraft and Rockets,2008,40(3):426-432.
  • 2Herrmann C R,Ingram G E,Welk E L.An application of the requirement vs capability analysis to estimating design reliability of solid rocket motors,NASA CR-1503[R].Houston:NASA Center,1970.
  • 3CHANG I-S,Patel N R,Yang S.Titan IV SRMU anomaly and redesign analyses,AIAA 94-3284[R].New York:AIAA:1994.
  • 4Bartolomey M.Overload test firings of propellant grains and their attachments to the motor case for large diameter rocket motors (Mechanical behavior),AIAA 80-1179[R].New York:AIAA:1980.
  • 5Davenas A.Solid rocket propulsion technology[M].London:Pergamon Press,1993.
  • 6Nahon S,Silivestrini P,Thepenier J.Probabilistic assessment for the design of high reliability objects (>0.999) such as solid propellant grains,AIAA 92-3359[R].New York:AIAA:1992.
  • 7Thepenier J,Gondouin B,Menez-Coutanceau H.Reli-ability of solid propellant grains:Mechanical analog motors and testing,AIAA 87-1987[R].New York:AIAA:1987.
  • 8Wang D T,Shearly R N.A review of solid propellant grain structural margin of safety evaluation methods,AIAA 86-1415[R].New York:AIAA:1986.
  • 9Majerus J N,Tamekuni H.The effect of material nonlinearity and failure criteria upon predicted propellant grain reliability,AIAA 65-158[R].New York:AIAA,1965.

同被引文献58

引证文献4

二级引证文献14

相关作者

内容加载中请稍等...

相关机构

内容加载中请稍等...

相关主题

内容加载中请稍等...

浏览历史

内容加载中请稍等...
;
使用帮助 返回顶部