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Study on Reduction of Reentry Blackout by Surface Catalysis Effect

Research Project

Project/Area Number 17K14871
Research Category

Grant-in-Aid for Young Scientists (B)

Allocation TypeMulti-year Fund
Research Field Aerospace engineering
Research InstitutionHokkaido University

Principal Investigator

Takahashi Yusuke  北海道大学, 工学研究院, 助教 (40611132)

Project Period (FY) 2017-04-01 – 2020-03-31
Project Status Completed (Fiscal Year 2019)
Budget Amount *help
¥4,290,000 (Direct Cost: ¥3,300,000、Indirect Cost: ¥990,000)
Fiscal Year 2019: ¥1,300,000 (Direct Cost: ¥1,000,000、Indirect Cost: ¥300,000)
Fiscal Year 2018: ¥1,430,000 (Direct Cost: ¥1,100,000、Indirect Cost: ¥330,000)
Fiscal Year 2017: ¥1,560,000 (Direct Cost: ¥1,200,000、Indirect Cost: ¥360,000)
Keywords惑星大気再突入 / 通信ブラックアウト低減化技術 / 表面触媒性 / 空力加熱 / プラズマ中の電磁波伝播 / アーク加熱風洞 / 通信ブラックアウト低減化 / 表面触媒効果 / 通信ブラックアウト / プラズマ流
Outline of Final Research Achievements

The radio frequency (RF) blackout for telecommunications between a reentry vehicle and a ground station hinders the accurate prediction of landing sites and increases the recovery cost. A mitigation method of RF blackout has been demanded. In this study, I proposed and demonstrated the new mitigation method using the surface catalysis effects with numerical simulation approach and wind tunnel experiments. The communication situation in reentry plasma was experimentally reproduced by 1 MW arc-heated wind tunnel, which generates high-temperature flows on the ground. Comparative tests were performed by two test models with high and low catalysis material of surfaces. The results indicated that the test model having high catalysis improves the communication situation, that is, mitigation of RF blackout. In addition, the mechanism to mitigating the RF blackout was clarified by the use of numerical analysis.

Academic Significance and Societal Importance of the Research Achievements

宇宙開発利用や小型衛星・超小型衛星の近年の進展から、宇宙から地上に資料などを持ち帰る需要や機会は増大していくと期待される。その際において地球大気再突入は避けて通れない過程である。再突入時において宇宙機は高速・高温の極限的環境に置かれ、強い空力加熱や空力不安定など様々な問題が生じる。通信ブラックアウトもその1つであり、高精度着地点予測の妨げになるとともに回収コストの増大を招く。本研究ではこの問題を緩和するために新しいブラックアウト低減化技術を提案実証し、メカニズム解明を行った。本成果はブラックアウト低減化だけでなくスピンオフとして表面触媒によるプラズマ制御技術につながることも期待される。

Report

(4 results)
  • 2019 Annual Research Report   Final Research Report ( PDF )
  • 2018 Research-status Report
  • 2017 Research-status Report
  • Research Products

    (26 results)

All 2020 2019 2018 2017

All Journal Article (7 results) (of which Int'l Joint Research: 1 results,  Peer Reviewed: 7 results,  Open Access: 1 results) Presentation (19 results) (of which Int'l Joint Research: 6 results,  Invited: 1 results)

  • [Journal Article] Aerothermodynamic analysis for deformed membrane of inflatable aeroshell in orbital reentry mission2019

    • Author(s)
      Takahashi Yusuke、Koike Taiki、Oshima Nobuyuki、Yamada Kazuhiko
    • Journal Title

      Aerospace Science and Technology

      Volume: 92 Pages: 858-868

    • DOI

      10.1016/j.ast.2019.06.047

    • Related Report
      2019 Annual Research Report
    • Peer Reviewed
  • [Journal Article] Drag Behavior of Inflatable Reentry Vehicle in Transonic Regime2019

    • Author(s)
      Takahashi Yusuke、Matsunaga Manabu、Oshima Nobuyuki、Yamada Kazuhiko
    • Journal Title

      Journal of Spacecraft and Rockets

      Volume: 56 Issue: 2 Pages: 577-585

    • DOI

      10.2514/1.a34069

    • NAID

      120006628714

    • Related Report
      2018 Research-status Report
    • Peer Reviewed
  • [Journal Article] Aerodynamic heating of inflatable aeroshell in orbital reentry2018

    • Author(s)
      Takahashi Yusuke、Yamada Kazuhiko
    • Journal Title

      Acta Astronautica

      Volume: 152 Pages: 437-448

    • DOI

      10.1016/j.actaastro.2018.08.003

    • NAID

      120006941682

    • Related Report
      2018 Research-status Report
    • Peer Reviewed
  • [Journal Article] Aerodynamic instability of flare-type membrane inflatable vehicle in suborbital reentry demonstration2018

    • Author(s)
      OHASHI Tatsushi、TAKAHASHI Yusuke、TERASHIMA Hiroshi、OSHIMA Nobuyuki
    • Journal Title

      Journal of Fluid Science and Technology

      Volume: 13 Issue: 3 Pages: JFST0020-JFST0020

    • DOI

      10.1299/jfst.2018jfst0020

    • NAID

      130007496913

    • ISSN
      1880-5558
    • Related Report
      2018 Research-status Report
    • Peer Reviewed
  • [Journal Article] Reentry blackout prediction for atmospheric reentry demonstrator mission considering uncertainty in chemical reaction rate model2018

    • Author(s)
      Jung Minseok、Kihara Hisashi、Abe Ken-ichi、Takahashi Yusuke
    • Journal Title

      Physics of Plasmas

      Volume: 25 Issue: 1 Pages: 013507-013507

    • DOI

      10.1063/1.5010713

    • Related Report
      2017 Research-status Report
    • Peer Reviewed
  • [Journal Article] Plasma flow modeling for Huels-type arc heater with turbulent diffusion2017

    • Author(s)
      Takahashi Yusuke、Esser Burkard、Steffens Lars、Guelhan Ali
    • Journal Title

      Physics of Plasmas

      Volume: 24 Issue: 12 Pages: 123509-123509

    • DOI

      10.1063/1.5008909

    • NAID

      120006370618

    • Related Report
      2017 Research-status Report
    • Peer Reviewed / Open Access / Int'l Joint Research
  • [Journal Article] 柔軟エアロシェル大気圏突入機の空力加熱解析2017

    • Author(s)
      高橋裕介,松永学,大島伸行,山田和彦
    • Journal Title

      日本航空宇宙学会誌

      Volume: 65 Pages: 370-376

    • NAID

      130006247446

    • Related Report
      2017 Research-status Report
    • Peer Reviewed
  • [Presentation] Study on Mitigation of Reentry Blackout by Surface Catalysis Effects in Arc-Heated Wind Tunnel2020

    • Author(s)
      Hideto Takasawa, Yusuke Takahashi, Nobuyuki Oshima, Hisashi Kihara
    • Organizer
      Aerospace Europe Conference 2020,
    • Related Report
      2019 Annual Research Report
    • Int'l Joint Research
  • [Presentation] 1MW アーク加熱風洞における触媒再結合反応を用いた通信ブラックアウト低減化通信試験2019

    • Author(s)
      高澤秀人,高橋裕介,大島伸行,木原尚
    • Organizer
      令和元年度宇宙航行の力学シンポジウム
    • Related Report
      2019 Annual Research Report
  • [Presentation] 1MWアーク加熱風洞における通信ブラックアウト低減化の数値シミュレーション2019

    • Author(s)
      高澤秀人,高橋裕介,大島伸行,木原尚
    • Organizer
      第33回数値流体力学シンポジウム,
    • Related Report
      2019 Annual Research Report
  • [Presentation] アーク加熱風洞における通信ブラックアウト低減化の数値解析2019

    • Author(s)
      高澤秀人,高橋裕介,大島伸行
    • Organizer
      第51回流体力学講演会/第37回航空宇宙数値シミュレーション技術シンポジウム
    • Related Report
      2019 Annual Research Report
  • [Presentation] Aerodynamics of Inflatable Nano-Satellite “EGG” in Low Earth Orbit and Reentry Duration2018

    • Author(s)
      Naoya Enoki, Yusuke Takahashi, Nobuyuki Oshima, Kazuhiko Yamada and Kojiro Suzuki
    • Organizer
      31st Internal Symposium on Rarefied Gas Dynamics
    • Related Report
      2018 Research-status Report
    • Int'l Joint Research
  • [Presentation] ISAS 1MW アーク加熱風洞におけるアーク加熱気流について2018

    • Author(s)
      高橋裕介,榎尚也,木原尚,山田和彦,下田孝幸
    • Organizer
      平成30年度宇宙航行の力学シンポジウム
    • Related Report
      2018 Research-status Report
  • [Presentation] 観測ロケットを用いた再突入試験における柔軟構造体の空力安定性に関する研究2018

    • Author(s)
      大橋達志,高橋裕介,寺島洋史,大島伸行
    • Organizer
      日本機械学会流体工学部門講演会
    • Related Report
      2018 Research-status Report
  • [Presentation] 表面触媒性効果を用いた大気圏再突入時の通信途絶現象低減化に関する研究2018

    • Author(s)
      榎尚也,高橋裕介,寺島洋史,大島伸行
    • Organizer
      日本機械学会流体工学部門講演会
    • Related Report
      2018 Research-status Report
  • [Presentation] 柔軟構造再突入機の空力加熱について2018

    • Author(s)
      高橋裕介,小池太輝,大島伸行
    • Organizer
      日本機械学会2018年度年次大会
    • Related Report
      2018 Research-status Report
  • [Presentation] Aerodynamic Heating Prediction of Flare-type Membrane Inflatable Reentry Vehicle from Low Earth Orbit2018

    • Author(s)
      Taiki Koike, Yusuke Takahashi, Nobuyuki Oshima, and Kazuhiko Yamada
    • Organizer
      2018 AIAA Atmospheric Flight Mechanics Conference, AIAA SciTech Forum, (AIAA 2018-0289), AIAA
    • Related Report
      2017 Research-status Report
    • Int'l Joint Research
  • [Presentation] 大気再突入時における宇宙機の空力・空力加熱について2018

    • Author(s)
      高橋裕介,小池太輝
    • Organizer
      北海道大学-JAXA連携企画講演会・HASTIC学術技術講演会
    • Related Report
      2017 Research-status Report
    • Invited
  • [Presentation] Aerodynamic Instability of Flare-type Membrane Inflatable Vehicle in Suborbital Reentry Demonstration2017

    • Author(s)
      Tatsushi OHASHI, Manabu MATSUNAGA, Yusuke TAKAHASHI, Hiroshi TERASHIMA, Nobuyuki OSHIMA
    • Organizer
      The Ninth JSME-KSME Thermal and Fluids Engineering Conference (TFEC9)
    • Related Report
      2017 Research-status Report
    • Int'l Joint Research
  • [Presentation] Prediction of electromagnetic waves around an inflatable reentry vehicle in an atmospheric reentry mission2017

    • Author(s)
      Naoya ENOKI, Manabu MATSUNAGA, Yusuke TAKAHASHI, Hiroshi TERASHIMA, Nobuyuki OSHIMA, Kazuhiko YAMADA, Kojiro SUZUKI
    • Organizer
      The Ninth JSME-KSME Thermal and Fluids Engineering Conference (TFEC9)
    • Related Report
      2017 Research-status Report
    • Int'l Joint Research
  • [Presentation] Numerical Simulation of Plasma Flows and Radio-Frequency Blackout in Atmospheric Reentry Demonstrator Mission2017

    • Author(s)
      Minseok Jung, Hisashi Kihara, Ken-ichi Abe, and Yusuke Takahashi
    • Organizer
      47th AIAA Fluid Dynamics Conference, AIAA AVIATION Forum, AIAA paper 2017-3308, AIAA
    • Related Report
      2017 Research-status Report
    • Int'l Joint Research
  • [Presentation] 展開型柔軟構造エアロシェルの空力加熱解析2017

    • Author(s)
      小池太輝,高橋裕介,大島伸行,山田和彦
    • Organizer
      平成29年度宇宙航行の力学シンポジウム
    • Related Report
      2017 Research-status Report
  • [Presentation] 柔軟構造再突入体に対する再突入ブラックアウト評価2017

    • Author(s)
      榎尚也,高橋裕介,大島伸行
    • Organizer
      平成29年度宇宙航行の力学シンポジウム
    • Related Report
      2017 Research-status Report
  • [Presentation] 柔軟構造体に対する再突入ブラックアウトの数値解析2017

    • Author(s)
      榎尚也,松永学,高橋裕介,寺島洋史,大島伸行
    • Organizer
      第49回流体力学講演会/第35回航空宇宙数値シミュレーション技術シンポジウム
    • Related Report
      2017 Research-status Report
  • [Presentation] 観測ロケットを用いた柔軟構造体の再突入試験における空力不安定性解析2017

    • Author(s)
      大橋達志,松永学,高橋裕介,寺島洋史,大島伸行
    • Organizer
      第49回流体力学講演会/第35回航空宇宙数値シミュレーション技術シンポジウム
    • Related Report
      2017 Research-status Report
  • [Presentation] 大気圏再突入用柔軟構造エアロシェルの空力加熱解析2017

    • Author(s)
      小池太輝,高橋裕介,大島伸行
    • Organizer
      第49回流体力学講演会/第35回航空宇宙数値シミュレーション技術シンポジウム
    • Related Report
      2017 Research-status Report

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Published: 2017-04-28   Modified: 2021-02-19  

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