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预冷却ATREX发动机主要部件发展研究 被引量:3

Development Study on Primary Components of the Pre-Cooled ATREX Engine
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摘要 文中分析了 ATREX 发动机模型和工作原理,介绍了其主要部件的研究和发展情况,与常规发动机相比说明了其发展的优势,总结归纳了这种发动机技术特点和发展的关键技术。研究认为 ATREX 发动机采用液态氢预冷却方式,大大扩展了常规涡轮发动机的工作范围,可满足高速飞行器或两级入轨空天飞机第一级动力装置的要求。 This paper analyzed to ATREX the work characteristics,explained its development advantage compare with the general engine,the summary induced this kind of engine technique characteristics and the key technique of the devel- opment.Drawing a conclusion by referencing the document published from aboard,similar to the ATREX,adopting liquid hydrogen cooler and pre-cooled method,can expand the regulations turbojet work scope consumedly,can satisfy the request of the supersonic aircraft of TSTO aircraft of the first stage equip.
出处 《弹箭与制导学报》 CSCD 北大核心 2004年第S6期313-315,共3页 Journal of Projectiles,Rockets,Missiles and Guidance
关键词 涡轮基发动机 预冷却 ATREX 发动机 高超音速飞行器 TBCC pre-cooled ATREX hypersonic aircraft
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参考文献6

  • 1Tetsuya Sato,Nobuhiro Tanatsugu.Developncnt Study Of The ATRTEX Engine For TSTO. AIAA 2001-1839 .
  • 2Konsuke,Jnsuke,Takeshi.A Feasibility Study of An ATREX Engine at Approved Technology Levels. AIAA 2001-1836 .
  • 3N.Tanatsugu,T.Sato,V.V.Balepin.Development Study on ATREX Engine. AIAA 96-4553 .
  • 4N.Tanatsugu,T.Honda.Development Study on Air Turbo-Ramjet for Future Space Plane. IAF 89-311 .
  • 5H.Konbayashi,N.Kanatsugu.Optimization Method on TSTO Spaceplane System Powered by Airbreather. AIAA 2001-3965 .
  • 6Isomura,Kousuke,Omi,Junsuke.A Comparative Study of an ATREX Engine and a Turbo Jet Engine. A01-34040,AIAA Paper 2001-3239 .

同被引文献64

  • 1商旭升,蔡元虎,肖洪.预冷却吸气式涡轮冲压膨胀循环发动机发展简介[J].兵工学报,2006,27(3):480-484. 被引量:4
  • 2Varvill R, Bond A. The skylon spaceplane [ J]. JBIS, 2004, 57:22 - 32.
  • 3Varvill R. Heat exchanger development at Reaction Engines Ltd [ J ]. Acta Astronautiea, 2010, 66 : 1468 - 1474.
  • 4Varvill R, Bond A. A comparison of propulsion concepts for SSTO reusable launchers [ J]. JBIS, 2003, 56:108 - 117.
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  • 6Hendfick P, Heintz N, Bizzarri D. Air-hydrogen heat exchangers for advanced space launchers [ J ]. Journal of Propulsion and Power, 2009, 25:1211 - 1219.
  • 7Bums B R A. HOTOL space transport for the twenty first century [ J ]. Proceedings of the Institute of Mechanical Engineers, 1990, 204:101 - 110.
  • 8Carter P H. Mass injection and precompressor cooling engines analyses [ C ]. 8th AIAA/ASME/SAE/ASEE Joint Propulsion Conference & Exhibit, Indianapolis, Indiana, 2002.
  • 9Balepin V V, Maita M, Murthy S N B. Third way of development of single-stage-to-orbit propulsion [ J ]. Journal of Propulsion and Power, 2000, 16:99 - 104.
  • 10Sato T, Tanatsugu N, Naruo Y, et al. Development study on ATREX engine [ J]. Acta Astronautica, 2000:799 - 808.

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