摘要
固体火箭发动机具有结构简单、可靠性高、便于机动部署和快速响应等优点,是战略/战术导弹武器的主要动力装置和航天运载火箭系统的重要动力源。介绍了世界各国现役典型固体火箭发动机及其采用的先进技术,分析了西方航天强国与我国的固体火箭推进技术发展水平与差距。针对我国航天发展及国防装备需求,提出了固体火箭推进技术如何发展、研发工作如何开展若干问题的几点思考,为我国固体火箭推进技术研究提供参考。
Due to the advantages including inherent simplicity,high reliability,convenience for maneuver deployment and quick response,solid rocket motors play an important role in power plants of the strategic/tactical missiles and space launch vehicle.Typi⁃cal solid rocket motors in service together with their advanced technologies were introduced.The development and difference in the field of solid rocket propulsion technology between Western aerospace powers and China were analyzed.In accordance with the re⁃quirements of aerospace development and national defense equipment updating,some suggestions on the development of solid rocket propulsion technology and how to carry out the relevant research were proposed,aiming to provide reference for the development of solid rocket propulsion technology.
作者
叶定友
薛朋飞
闫大庆
YE Dingyou;XUE Pengfei;YAN Daqing(The Fourth Academy of CASC,Xi'an 710025,China;Xi'an Institute of Aerospace Information,Xi'an 710025,China)
出处
《固体火箭技术》
CAS
CSCD
北大核心
2021年第4期427-430,共4页
Journal of Solid Rocket Technology
关键词
固体火箭发动机
设计优化
精细化
能量管理
智能化
使用性能
solid rocket motor
design optimization
refined design
energy management
artificial intelligenee
serviceability
