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2000年巡航弹用小涡轮发动机
引用本文:王培林.2000年巡航弹用小涡轮发动机[J].推进技术,1989,10(5):1-5,71.
作者姓名:王培林
作者单位:航空航天部三院31所
摘    要:本文简要评述了国外当前弹用小发动机的设计特点,描述了2000年弹用小涡轮发动机的发展概貌,还介绍了未来弹用小发动机发展的材料、空气动力学和结构技术三方面的关键技术.

关 键 词:空气喷气发动机  巡航导弹

SMAII GAS TURBINE ENGINES FOR CRUISE MISSILES IN 2000
Wang Pailin.SMAII GAS TURBINE ENGINES FOR CRUISE MISSILES IN 2000[J].Journal of Propulsion Technology,1989,10(5):1-5,71.
Authors:Wang Pailin
Institution:The 31st Research Institute
Abstract:A brief review on basic design features of nowaday small engines for cruise missiles in foreign countries and their further development are described in this paper. The key technologies of further small turbine engine for cruise missiles such as materials, aerodynamics and structures are discussed emphatically.
Keywords:Air breathing engine  Cruise missile  
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