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Wind Tunnel Testing for Air-breathing Engines of Space Planes

Research Project

Project/Area Number 10044187
Research Category

Grant-in-Aid for Scientific Research (B).

Allocation TypeSingle-year Grants
Section一般
Research Field Aerospace engineering
Research InstitutionInstitute of Space and Astronautical Science

Principal Investigator

TANATSUGU Nobuhiro  Institute of Space and Astronautical Science (ISAS), Research Division for Space Propulsion, Professor, 宇宙推進研究系, 教授 (70013737)

Co-Investigator(Kenkyū-buntansha) ARAI Takakage  Muroran Institute of Technology, Department of Mechanical System Engineering, Associate Professor, 工学部, 助教授 (10175945)
ABC Takashi  Institute of Space and Astronautical Science ISAS, Research Division for Space Transportation, Professor, 宇宙輸送研究系, 教授 (60114849)
KUBOTA Hirotoshi  Univ.of Tokyo, Faculty of Engineering, Professor, 工学部, 教授 (30114466)
SATO Tetsuya  Institute of Space and Astronautical Science ISAS, Research Division for Space Propulsion, Research Associate, 宇宙推進研究系, 助手 (80249937)
NARUO Yoshihiro  Institute of Space and Astronautical Science ISAS, Research Division for Space Applications, Research Associate, 衛星応用工学研究系, 助手 (70150050)
Project Period (FY) 1998 – 2000
Project Status Completed (Fiscal Year 2000)
Budget Amount *help
¥6,500,000 (Direct Cost: ¥6,500,000)
Fiscal Year 2000: ¥2,300,000 (Direct Cost: ¥2,300,000)
Fiscal Year 1999: ¥2,000,000 (Direct Cost: ¥2,000,000)
Fiscal Year 1998: ¥2,200,000 (Direct Cost: ¥2,200,000)
KeywordsSpace Planes / Air-breathing Engine / Air-Turbo Ramjet Engine / Air Inlet / Catalytic Ignition / Supersonic Wind Tunnel Test / 触媒燃焼 / 乱流混合 / マッハ数スイープ
Research Abstract

Wind tunnel test methods on the air-breathing engine for the reusable space planes were researched under the actual flight conditions. A control method of the air-inlet by adjusting its shape was proposed and confirmed in the ONERA S3 supersonic wind tunnel. This test was successfully conducted in the variable Mach number conditions, which simulated the accelerating and decelerating conditions of the actual flight. An unsteady control method when the compression form changed was established. Some problems were cleared by comparing with the CFD analysis. Now the inlet control test with a small turbojet engine for a model plane in the supersonic wind tunnel is planned. The control scquences including in case of the inlet unstart and restart will be constructed in the test. As for the total engine system, the firing test of the air-turbo-ram jet engine was conducted under the sea-level static. The frost formation problem was especially investigated in the test and countermeasures against it were proposed and verified. Some lobe type mixers were tested in the ram combustor test. Platinum catalytic igniters were also tried in this combustion test, which was cooperated with ENSMA in France. We reserached some wind tunnels and measurement systems in USA, France and also discussed with foreign research on the future overall engine testing in the supersonic and hypersonic wind tunnel.

Report

(4 results)
  • 2000 Annual Research Report   Final Research Report Summary
  • 1999 Annual Research Report
  • 1998 Annual Research Report
  • Research Products

    (30 results)

All Other

All Publications (30 results)

  • [Publications] T.Sato,N.Tanatsugu,ET,AL.: "Development Study on ATREX Engine"Acta Astronautica. 47・11. 799-808 (2000)

    • Description
      「研究成果報告書概要(和文)」より
    • Related Report
      2000 Final Research Report Summary
  • [Publications] K.Harada,N.Tanatsugu,ET,AL.: "Development Study of a Precooler for the Air-Turboramjet Expander-Cycle Engine"Journal of Propulsion and Power. 17・5(掲載予定). (2001)

    • Description
      「研究成果報告書概要(和文)」より
    • Related Report
      2000 Final Research Report Summary
  • [Publications] T.Kojima,N.Tanatsugu,ET,AL.: "Experimental Study On Inlet Control system for Hypersonic Flight"22nd International Symposium on Space Technology and Science. (2000)

    • Description
      「研究成果報告書概要(和文)」より
    • Related Report
      2000 Final Research Report Summary
  • [Publications] 新井隆景,永田晴紀 他: "定温触媒線を用いた触媒燃焼による超音速乱流混合の評価方法"日本機械学会論文集(B編). 64・619. 793-799 (1998)

    • Description
      「研究成果報告書概要(和文)」より
    • Related Report
      2000 Final Research Report Summary
  • [Publications] 佐藤哲也,高木郁男 他: "超音速機用軸対称型エアインテークの実験研究"日本航空宇宙学会誌. 46. 539-544 (1998)

    • Description
      「研究成果報告書概要(和文)」より
    • Related Report
      2000 Final Research Report Summary
  • [Publications] 綿貫忠晴,久保田弘敏 他: "ソニックブーム強度に対する機体形状効果"日本航空宇宙学会誌. 47. 348-353 (1999)

    • Description
      「研究成果報告書概要(和文)」より
    • Related Report
      2000 Final Research Report Summary
  • [Publications] T.Sato, N.tanatsugu, ET, AL.: "Development Study on ATREX Engine"Acta Astronautica. Vol.47, No.11. 799-808 (2000)

    • Description
      「研究成果報告書概要(欧文)」より
    • Related Report
      2000 Final Research Report Summary
  • [Publications] K.Harada, N.Tanatsugu, ET, AL.: "Development Study of a Precooler for the Air-Turboramjet Expander-Cycle Engine"Journal of Propulsion and Power. Vol.17, No.5 (Scheduled). (2001)

    • Description
      「研究成果報告書概要(欧文)」より
    • Related Report
      2000 Final Research Report Summary
  • [Publications] T.Kojima, N.Tanatsugu, ET, AL.: "Experimental Study On Inlet Control System for Hypersonic Flight"Proceeding of 22nd Intermational Symposium on Space Technology and Science. (2000)

    • Description
      「研究成果報告書概要(欧文)」より
    • Related Report
      2000 Final Research Report Summary
  • [Publications] T.Arai, H.Nagata, et.al.: "Evaluation of Supersonic Turbulent Mixing Using Catalytic Combustion of Constant Temperature P1 Wire"Journal of the Janpan Society of Mechanical Engineering (B). Vol.64, No.619. 793-799 (1998)

    • Description
      「研究成果報告書概要(欧文)」より
    • Related Report
      2000 Final Research Report Summary
  • [Publications] T.Sato, I.Takagi, ET, AL.: "Experimental Study on Axisymmetric Air Intake for the Supersonic Transport"Journal of the Japan Society for Aeronautical and Space Sciences. Vol.48. 539-544 (1998)

    • Description
      「研究成果報告書概要(欧文)」より
    • Related Report
      2000 Final Research Report Summary
  • [Publications] T.Watanuki, H.Kubota, ET, AL.: "Effect of supersonic aircraft configuration on sonic-boom intensity-Near-field pressure distribution measurement"Journal of the Japan Society for Aeronautical and Space Sciences. Vol.47. 348-359 (1999)

    • Description
      「研究成果報告書概要(欧文)」より
    • Related Report
      2000 Final Research Report Summary
  • [Publications] T.Sato,N.Tanatsugu, ET,AL.: "Development Study on ATREX Engine"Acta Astronautica. 47・11. 799-808 (2000)

    • Related Report
      2000 Annual Research Report
  • [Publications] K.Harada,N.Tanatsugu, ET,AL.: "Development Study of a Precooler for the Air-Turboramjet Expander-Cycle Engine"Journal of Propulsion and Power. 17・5(掲載予定). (2001)

    • Related Report
      2000 Annual Research Report
  • [Publications] H.Kobayashi,N.Tanatsugu, ET,AL.: "Sizing Analysis for the TSTO Fly-back Booster Powered by ATREX Engines"51st International Astronautical Congress. (2000)

    • Related Report
      2000 Annual Research Report
  • [Publications] 佐藤哲也,棚次亘弘 他: "ATREXエンジンの研究開発状況"航空原動機・宇宙推進講演会講演集. 41. 56-61 (2001)

    • Related Report
      2000 Annual Research Report
  • [Publications] T.Sato,N.Tanatsugu, ET,AL.: "Development Study on the Precooler of ATREX Engine"22nd International Symposium on Space Technology and Science. (2000)

    • Related Report
      2000 Annual Research Report
  • [Publications] T.Kojima,N.Tanatsugu, ET,AL.: "Experimental Study On Inlet Control System for Hypersonic Flight"22nd International Symposium on Space Technology and Science. (2000)

    • Related Report
      2000 Annual Research Report
  • [Publications] 小島孝之、佐藤哲也他: "ATREXエアインテークの研究開発"航空原動機・宇宙推進講演会講演集. 40. 263-268 (2000)

    • Related Report
      1999 Annual Research Report
  • [Publications] 佐藤哲也、高木郁男他: "超音速機用軸対称型エアインテークの実験研究"日本航空宇宙学会誌. 46. 539-544 (1998)

    • Related Report
      1999 Annual Research Report
  • [Publications] 綿貫忠晴、久保田弘敏他: "ソニックブーム強度に対する機体形状効果"日本航空宇宙学会誌. 47. 348-353 (1999)

    • Related Report
      1999 Annual Research Report
  • [Publications] 佐藤哲也、棚次亘弘他: "ATREXエンジンプリクーラに関する研究"航空原動機・宇宙推進講演会講演集. 40. 245-250 (2000)

    • Related Report
      1999 Annual Research Report
  • [Publications] 新井隆景他: "超音速流中に垂直に噴出する噴流の挙動"航空原動機・宇宙推進講演会講演集. 40. 211-216 (2000)

    • Related Report
      1999 Annual Research Report
  • [Publications] T. Sato, N. Tanatsugu, ET, AL.: "Development Study on the Precooling System of ATREX Engine"50th International Astronautical Congress. (1999)

    • Related Report
      1999 Annual Research Report
  • [Publications] 佐藤哲也、高木郁男他: "超音速機用軸対称型エアインテークの実験研究" 日本航空宇宙学会誌. 46・539. 651-659 (1998)

    • Related Report
      1998 Annual Research Report
  • [Publications] 小林弘明、佐藤哲也: "極超音速飛翔体の機体予圧縮に関する数値解析" 日本航空宇宙学会誌. 46・532. 303-310 (1998)

    • Related Report
      1998 Annual Research Report
  • [Publications] 佐藤哲也、棚次亘弘他: "プリクーラを装着したATREXエンジンの地上燃焼試験" 航空原動機・宇宙推進講演会講演集. 39. 108-113 (1999)

    • Related Report
      1998 Annual Research Report
  • [Publications] 小島孝之、棚次亘弘他: "超音速エアーインテークの遷音速領域における性能向上について" 航空原動機・宇宙推進講演会講演集. 39. 353-358 (1999)

    • Related Report
      1998 Annual Research Report
  • [Publications] 新井隆景,永田晴紀他: "定温触媒線を用いた触媒燃焼による超音速乱流混合の評価方法" 日本機械学会論文集(B編). 64・619. 793-799 (1998)

    • Related Report
      1998 Annual Research Report
  • [Publications] T.Arai, et.al.: "Evaluation of Supersonic Turbulent Mixing Using Catalytic Combustion of Constant Temperature Pt Wire" JSME International Journal. 42・1. 65-70 (1999)

    • Related Report
      1998 Annual Research Report

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Published: 1998-04-01   Modified: 2016-04-21  

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