| 弹用涡喷、涡扇发动机发展概况 |
| |
| 引用本文： | 郑涛. 弹用涡喷、涡扇发动机发展概况[J]. 推进技术, 1995, 16(1): 7-12 |
| |
| 作者姓名： | 郑涛 |
| |
| 作者单位： | 航天工业总公司３１所 |
| |
| 摘 要： | 介绍了飞航式导弹主要动力装置的弹用涡喷、涡扇发动机的发展概况，包括发展历史、特点、技术现状，并论述了发展趋势。
|
| 关 键 词： | 巡航导弹 涡轮喷气发动机 透平风扇发动机 |
AN INTRODUCTION TO DEVELOPMENT OF TURBOJET AND TURBOFAN ENGINES FOR MISSILES |
| |
| Zheng Tao. AN INTRODUCTION TO DEVELOPMENT OF TURBOJET AND TURBOFAN ENGINES FOR MISSILES[J]. Journal of Propulsion Technology, 1995, 16(1): 7-12 |
| |
| Authors: | Zheng Tao |
| |
| Affiliation: | The 31st Research Iust. Beijing, 100074 |
| |
| Abstract: | The development of turbojet and turbofan engines used as cruisemissile's main propulsion are discribed, including their histories, characteristics andtechnical status. A prospects of these engines are also discussed. |
| |
| Keywords: | ruise missile Turbojet engine Trubofan engine Trend analysis |
| 本文献已被 CNKI 维普 等数据库收录！ |
| 点击此处可从《推进技术》浏览原始摘要信息 |
|
点击此处可从《推进技术》下载免费的PDF全文 |
