拦截器轨控发动机点火器分析与评估  

Analysis and Review of Orbital Control Rocket Motor Ignitor for Interceptor

作　　者：李逢春[1] 

机构地区：[1]西北工业大学,西安710072

出　　处：《固体火箭技术》1993年第4期21-26,共6页Journal of Solid Rocket Technology

摘　　要：对美国空基拦截器用轨控发动机组(MMA)的点火器性能特点、结构与材料等,进行了较全面的分析和评估,而且分析了该点火器在我国研制的可能性.开展此项研究,对我国战略防御武器系统的研究、设计和制造,将会产生较大的促进作用.An orbital control rocket motor ignitor for air-launched interceptor of US,ma-neuver motor array ignitor is called“MMA”ignitor for short.A detail analysis and reviewof its performance features,construction and materials ets.are presented.The feasibility ofresearch and development of the MMA ignitor at home is suggested.carrying out the re-search will greatly promote our research,designation and manufactory of strategic defenseweaponry system.

关 键 词：火箭发动机 点火装置 拦截器 

分 类 号：TJ760.3[兵器科学与技术—武器系统与运用工程]