| 国外高超声速组合推进技术概述 |
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| 引用本文： | 文科,李旭昌,马岑睿,宋亚飞.国外高超声速组合推进技术概述[J].航天制造技术,2011(1). |
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| 作者姓名： | 文科 李旭昌 马岑睿 宋亚飞 |
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| 作者单位： | 空军工程大学导弹学院; |
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| 摘 要： | 推进技术是高超声速武器的核心技术,以超燃冲压发动机为基础的高超声速组合推进技术是高超声速武器的首选动力方案。本文介绍了几种以超燃冲压发动机为基础的组合推进方案,并简要介绍了美国、日本以及印度的技术发展现状。
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| 关 键 词： | 超燃冲压发动机 高超声速 组合推进 RBCC TBCC |
Hypersonic Combined-cycle Propulsion Technology Based on Scramjet |
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| Wen Ke Li Xuchang Ma Cenrui Song Yafei.Hypersonic Combined-cycle Propulsion Technology Based on Scramjet[J].Aerospace Manufacturing Technology,2011(1). |
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| Authors: | Wen Ke Li Xuchang Ma Cenrui Song Yafei |
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| Institution: | Wen Ke Li Xuchang Ma Cenrui Song Yafei(Air Force Engineer University Missile Institute,Sanyuan 713800) |
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| Abstract: | Propulsion technology is the key of hypersonic weapons,which take hypersonic combined-cycle propulsion technology based on scramjet as the first choice scheme.This paper introduces some schemes and briefly summarizes the development of propulsion technology in America,Japan and India. |
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| Keywords: | scramjet hypersonic combined-cycle propulsion RBCC TBCC |
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