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.
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.
出处
《推进技术》
EI
CAS
CSCD
北大核心
1989年第5期1-5,共5页
Journal of Propulsion Technology
关键词
喷气发动机
巡航导弹
Air breathing engine, Cruise missile
