| X-51A超燃冲压发动机及飞行验证计划 |
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| 引用本文： | 曾慧,白菡尘,朱涛.X-51A超燃冲压发动机及飞行验证计划[J].导弹与航天运载技术,2010(1). |
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| 作者姓名： | 曾慧 白菡尘 朱涛 |
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| 作者单位： | 中国空气动力研究与发展中心超高速所,绵阳,622663;中国空气动力研究与发展中心超高速所,绵阳,622663;中国空气动力研究与发展中心超高速所,绵阳,622663 |
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| 摘 要： | 美国空军研究试验室(AFRL)/国防部预研局(DARPA)联合推出的X-51超燃冲压发动机演示器—乘波体(SED-WR)飞行器是美国空军研究试验室高超声速技术项目(HyTech)的飞行验证计划。对X-51A计划进行一个全面综述,主要叙述X-51A飞行器和推进系统的外形、完成计划情况以及还未展开的飞行试验计划等。
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| 关 键 词： | 超燃冲压发动机 高超声速 巡航导弹 |
X-51A Scramjet Engine Flight and Demonstration Program |
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| Zeng Hui,Bai Hanchen,Zhu Tao.X-51A Scramjet Engine Flight and Demonstration Program[J].Missiles and Space Vehicles,2010(1). |
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| Authors: | Zeng Hui Bai Hanchen Zhu Tao |
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| Affiliation: | China Aerodynamic Research & Development Center;Mianyang;622663 |
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| Abstract: | The joint Air Force Research Laboratory (AFRL)/Defense Advanced Research Projects Agency (DARPA) X-51A Scramjet Engine Demonstrator-WaveRider (SED) vehicle is the flight demonstration of AFRL's Hypersonic Technology(HyTech) program.An overview of the X-51A program is systematically summarized.focusing on the X-51A vehicle and propulsion system configurations,program accomplishments and plan for the future flight test activities. |
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| Keywords: | Scramjet engine Hypersonic Cruise missile |
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