安部・船木研究室

発表論文等 〜大気突入/惑星探査技術についての代表的な発表論文です〜

*惑星間航行技術に関する論文はこちらから。

<2008年度>

  1. M. Kawamura, A. Matsuda, H. Katsurayama, H. Otsu, D. Konigorski, S. Sato and T. Abe,
    :"Experimental study on drag enhancement for a blunt body with electrodynamic heat-shield,"
    :to be published, Journal Spacecraft and Rocket, (2009)
  2. T. Abe,
    :"Feasibility study of flight experiment for electrodynamic heatshield technology",
    :Acta Astronautica, to be published, (2009).
  3. T. Abe,
    : "Electrodynamic Heat-shield Technology - from basic research to applications,"
    :17th International Conference for Magneto-Hydro-dynamics, at Hayama, in Sep. (2009) (招待講演)
  4. T. Abe,
    : "A Review of MHD Research in Japan,"
    :CEAS (Council of Euroean Aerospace Societies) 2009 European Air and Space conference, at Manchester, (2009). (招待講演)
  5. T. Abe,
    : "Application of Bulk Superconductor to Space Reentry Flight,"
    :22nd International Symposium on Superconductivity, (2009). (招待講演)
  6. T. Abe,
    : "Atmospheric Reentry Spacecraft Environment and Heatshield Development",
    : International Workshop on Warm Dense Matter, in Hakone, (2009) (招待講演)
  7. K. Yamada, D. Akita, E. Sato, K. Suzuki, T. Narumi, T. Abe,
    :"Flare-Type Membrane Aeroshell Flight Test at Free Drop from a Balloon,"
    :Journal of Spacecraft and Rockets, vol.46, pp.606-614, (2009)
  8. H. Katsurayama, M. Kawamura, A. Matsuda, and T. Abe,
    :"Kinetic and Continuum Simulations of Electromagnetic Control of a Simulated Reentry Flow,"
    :Journal of Spacecraft and Rockets 2008, vol.45 no.2 (248-254). (査読論文)
  9. T. Abe, Y. Takizawa, S. Sato, N. Kimura,
    :"Experimental Study for Momentum Transfer in a Dielectric Barrier Discharge Plasma Actuator,"
    :AIAA Journal 2008, vol.46 no.9 (2248-2256). (査読論文)
  10. A.Matsuda, T.Tanifuji, K. Wasai, H. Yamasaki, T. Abe, H. Otsu, D. Konigorski,
    :"Expansion Tube Experiment of Applied Magnetic Field Effect on Reentry Plasma,"
    :AIAA Paper-2008-1113, 2008. (査読無)
  11. H. Otsu, Y. Yamagiwa, T. Abe, D. Konigorski, A. Nakamura,
    :"Application of the Magnetic Flow Control System for Aerobraking Flight of the Reentry Vehicle,"
    :AIAA Paper-2008-3897, , 2008. (査読無)
  12. T. Abe, S Sato, K Taguchi, Y Tamura,
    :"Acoustic Wave Analysis for a DBD Plasma Actuator,"
    : AIAA Paper-2008-3795, 2008. (査読無)
  13. H. Katsurayama, T. Abe, D. Konigorski,
    :"Numerical Simulation of Electromagnetic Flow Control in a One-Kilowatt Class Argon Arcjet WIndtunnel,"
    : AIAA Paper-2008-4016, 2008.(査読無)
  14. T. Tanifuji, K. Wasai, D. Konigorski, T. Abe, H. Makino, H. Otsu, M. Furudate, Hiroyuki Yamasaki,
    :"Experimental Investigation of Electrodynamic Heatshield Effect in a Reentry Plasma,"
    :AIAA Paper-2008-3789, 2008. (査読無)
  15. H. Katsurayama, T. Abe, D. Konigorski,
    :"Numerical Simulation of Electromagnetic Flow Control in an Arcjet Plume,"
    :AIAA Paper-2008-1392, 2008. (査読無)
  16. A. Matsuda, H. Otsu, M. Kawamura, Y. Takizawa, D. Konigorski,T. Abe,
    :"Model and magnetic configuration effect on the shock layer enhancement by an applied magnetic field,"
    :Physics of Fluids, vol.20, No.2, pp 027102-1 - 027102-11 , 2008. (査読論文)


<2007年度>

  1. T. Tanifuji, A. Matsuda, K. Wasai, H. Otsu, H. Yamasaki, D. Konigorski and T. Abe
    :Expansion tube experiment of applied magnetic field effect on reentry plasma
    :46th AIAA Aerospace sciences Meeting and Exhibit:AIAA 2008-1113: USA:(2008)
  2. H. Otsu, T. Matsumura, Y. Yamagiwa (Shizuoka Univ.), A. Matsuda (Nagoya Univ.), T. Abe (ISAS/JAXA), M.Kawamura (Univ. of Tokyo) and D. Konigorski (EADS)
    :Effect of Nose Bluntness on the Electromagnetic Flow Control for Reentry Vehicles:Proceedings of the 26th International Symposium on Shock Waves
    :in press:USA:(2007)
  3. H. Katsurayama, T. Abe, H. Otsu and D. Konigorski
    :Numerical Study of the Electromagnetic Control of a Weakly Ionized Flow around a Blunt Body: Role of a Insulative Boundary in the Flow
    :38th AIAA Plasmadynamics and Lasers Conference:AIAA-2007-4529:USA:(2007)
  4. H. Katsurayama, A. Matsuda and T. Abe
    :Preliminary Investigation of Thermochemical Nonequilibrium behind a Strong Shock Wave with Precursor Photoionization in Argon
    :39th AIAA Thermophysics Conference:AIAA-2007-4552:USA:(2007)
  5. H. Katsurayama, M. Kawamura, A. Matsuda and T. Abe
    :Kinetic and Continuum Simulations of Electromagnetic Control of a Simulated Reentry Flow:Journal of Spacecraft and Rockets
    :in press:(2008)
  6. M. Kawamura, A. Matsuda, H. Katsurayama, H. Otsu, Detlev Konigorski, T. Abe
    :Experimental Study on Electromagnetic Drag Increment of Blunt Body in a Weakly Ionized Plasma Flow
    :38th AIAA Plasma dynamics and Laser Conference:AIAA-2007-3889:USA:(2007)
  7. T. Abe
    :DBD plasma actuator and Elecctrodynamic heat shield --possible flow control technique by an electro-magnetic means
    :The Fourth International Conference on Flow Dynamics September 26-28, 2007:(2007)
  8. T. Abe
    :Electrodynamic Heat Shield Effect for a Magnetized Blunt Body in a Weakly-ionized Flow at Reentry Condition
    :2007 AEROSPACE THEMATIC WORKSHOP “Fundamentals of Aerodynamic-Flow and Combustion Control by Plasmas”:Italy:(2007)
  9. Atsushi Matsuda, Hirotaka Otsu, Masaaki Kawamura, Yuji Takizawa, Detlev Konigorski, Takashi Abe
    :Model and magnetic configuration effect on the shock layer enhancement by an applied magnetic field
    :Physics of Fluids:Vol.20, No.2, pp 027102.1-027102.11:(2008)
  10. Atsushi Matsuda, Masanori Ota, Suhe Batter, Keishi Arimura, Kazuo Maeno, Takashi Abe
    :Ro-Vibrational Temperatures Derived from N2(2+) Emission Spectra and CARS Method behind Strong Shock Waves
    :Thermophysics Conference:AIAA 2007-4547:USA:(2007)
  11. Yuji Takizawa, Atsushi Matsuda, Shunichi Sato, Takashi Abe
    :Optical Investigation of Discharge Structure of DBD Plasma Actuator:Plasmadynamics and Laser Conference
    :AIAA 2007-4376:USA:(2007)
  12. Atsushi Matsuda, Masanori Ota, Keishi Arimura, Suhe Bater, Kazuo Maeno and Takashi Abe
    :Assessment of rotational and vibrational temperatures behind strong shock waves derived from CARS method
    :26th International Symposium on Shock Waves:ISSW-2981:Germany:(2007)


<2005年度>

  1. M. Furudate, K. Fujita and T. Abe, "Coupled Rotational-Vibrational Relaxation of Molecular Hydrogen at High Temperature," Journal of Thermophysics and Heat Transfer, in press, (2005).
  2. Hirotaka Otsu, Takashi Abe, and Detlev Konigorski, "Influence of the Hall Effect on the Electrodynamic Heat Shield System for Reentry Vehicles," AIAA2005-5049, (2005).
  3. Atsushi Matsuda, Kazuhisa Fujita, Shunichi Sato and Takashi Abe, "Absorption Spectroscopy for Temperature Measurement Behind Shock Wave at Super-Orbital Velocity," JOURNAL OF THERMOPHYSICS AND HEAT trANSFER, Vol.19, No.3, July September2005
  4. Nobuyoshi Komatsu, and Takashi Abe, "Shape effect of hot droplets on fragmentation," PHYSICAL REVIEW E 72, 021601, (2005).
  5. Nobuyoshi Komatsu and Takashi Abe, "Noise-driven numerical irreversibility in molecular dynamics technique," Computer Physics Communications Vo.171, pp.187-196, (2005).
  6. Yuji Takizawa, Atsushi Matsuda, Shunichi Sato, Takashi Abe and Detlev Konigorski, "Experiment on Shock Layer Enhancement by Electro-magnetic Effect in Reentry-related High-enthalpy Flow," AIAA 36th Plasmadynamics and Laser Conference, AIAA2005-4786, Toronto(on), CANADA, June (2005).

<2004年度>

  1. Takashi Abe, Yuji Takizawa, Hirotaka Otsu, Detlev Konigorski, "Possiblity of Electro-magnetic Heat Shield for Reentry Vehicle, " First Int. Conf. Flow Dynamics : Int. COE of Flow Dynamics, Tohoku Univ. : (2004).
  2. Takashi Abe, "Recent activities related to Reentry technology at ISAS," 2nd Radiation Work Shop : ESTEC : (2004).
  3. Nobuyoshi Komatsu and Takashi Abe, "Numerical Irreversibility in Time-Reversible Molecular Dynamics Simulation," Physica D, (2004).
  4. Nobuyoshi Komatsu and Takashi Abe, "Noise-Driven Numerical Irreversibilty in Molecular Dynamics Technique," Comput. Phys. Comm, (2005).
  5. Nobuyoshi Komatsu and Takashi Abe, "Noise-Driven Numerical Irreversibility in Time-Reversible Molecular Dynamics Simulation," CCP2004, Conference on Computational Physics, ヨーロッパ物理学会,アメリカ物理学会,(2004).
  6. Nobuyoshi Komatsu and Takashi Abe, "Noise-driven Numerical irrerversibility in Time-reversible molecular dynamics simulation," Workshop on Chaos and Nonlinear Dyanmics in Quantum-Mechanical and Macroscopic Systems, 京大基礎物理学研究所,(2004).
  7. Atsushi Matsuda, Kazuhisa Fujita, Shunichi Sato, and Takashi Abe, "Experimental Investigation of the Shock Layer Associated with the Super-orbital Reentry Velocity," 24th International Symposium on Space Technology and Science, (2004).
  8. Atsushi Matsuda, Kazuhisa Fujita, Shunichi Sato, and Takashi Abe, "Nonequilibrium Phenomena Behind Strong Shock Waves Generated in Superorbital Reentry Flight," Journal of Thermophysics and Heat Transfer, American Institute of Aeronautics and Astronautics, (2004).
  9. Noriaki Tsuzuki, Shunichi Sato, and Takashi Abe, "Conceptual Design and Feasibility for a Miniature Mars Exploration Rotorcraft," 24th ICAS, (2004).
  10. Yuji Takizawa, Takashi Abe, "Electro-magnetic effect on shock layer structure in reentry-related high-enthalpy flow," AIAAPlasmadynamics and Lasers Conference, AIAA(2005).
  11. Eiji Sato, Kazuhiko Yamada, Kojiro Suzuki, Takashi Abe, Daisuke Akita, Eiko Nakazawa, Masafumi Kiuchi, Yuki Tsutsumi, Kazuhiko Wakatsuki, Akira Sakurai, Tomohiro Narumi, Yukihiko Matsuzaka, Issei Iijima, "Flight Experiment of Capsule-Type Vehicle with Membrane Aeroshell by means of Large Scientific Balloon," 24th International Symposium on Space Technology and Science, (2004).
  12. Eiji Sato, Shunichi Sato, Takashi Abe, "Interaction Between Shock Wave and Glow Discharge Plasmas," 43rd AIAA Aerospace Sciences Meeting and Exhibit, American Institute of Aeronautics and Astronautics, (2005).

<2003年度>

  1. K. Fujita, S. Sato, T. Abe, H. Otsu, "Electron Density Measurements Behind Strong Shock Waves by H-_ Profile Matching," Journal of Thermophysics and Heat Transfer, Vol.17, No.22, pp.210-216 (2003).
  2. A. Matsuda, K. Fujita, S. Sato and T. Abe, "Translational Temperature Measurement for Atomic Oxygen Behind Shock Waves by Absorption Spectroscopic Techniqne," 36th AIAA Thermophysics Conference, AIAA2003-3784, (2003).
  3. Y. Takizawa, S. Sato, K. Fujita, T. Abe and D. Konigorski, "Electro-magnetic Effect on a Reentry-related Highenthalpy Flow," 34th AIAA Plasmadynamics and Lasers Conference : Orlando : AIAA2003-4168, (2003).
  4. K. Fujita and T. Abe, "Coupled Rotatina-Vibratin-Dissociation Kinetics of Nitrogen Using QCT Models," AIAA2003-3779, (2003).
  5. M. Furudate, K. Fujita, T. Abe, "Coupled Rotational-Vibrational Relaxation of Molecular Hydorogen at High Temperature," AIAA2003-3780, (2003).
  6. K. Fujita, Y. Inatani, K. Hiraki, T. Abe, "Assessment of Dynamis Stability of MUSES-C Capsule oin Hypersonic Rarefied Regime," AIAA2003-3893, (2003).
  7. Takashi Abe, Yuji Takizawa, Shunichi Sato, Detlev Konigorski, "Electro-magnetic shield effect on reentry-related high-enthalpy," Proc. of International Conference on Recent Advences in Space Technologgies, at Istanbul, (2003).
  8. Takashi Abe, Shunichi Sato, Yutaka Matsukawa, Kazushi Yamamoto and Kazumi Hiraoka, "Study for dynamically unstable pitching motion of reentry capsule," CFD Journal Vol.12, No.4, (2003).

<2002年度>

  1. Matsuda, A., Fujita, K., Sato. S., and Abe, T., "Experimental Study of Nonequilibrium Phenomena of Shock Layer Generated by Super-Orbital Re-entry flight," Proceedings of the 23rd International Symposium on Space Technology and Science, Matue, Japan, (2002).
  2. Fujita, K. and Abe, T., "Rotational State-to-state Relaxation and Dessoiation of Nitrogen behind a Strong Shock Wave," Proceedings of the 23rd Internaional Symposium on Space Technology and Science, Matsue, Japan, (2002).
  3. Fujita, K., Sato, S., Abe, T., and Otsu, H., "Electron Density Measurements behind Strong Shock Waves by H Beta Profile Matching," Journal of Thermophysics and Heat Transfer, (accepted for publication in Vol.17, No.1, 2003).
  4. Matsushita, K., Abe, T., "Control of Aerodynamic Heating in Hypersonic Plasma by Magnetic Field," Proceedings of the 23rd International Symposium on Space Technology and Science, Matsue, Japan, (2002).
  5. Matsuda, A., Fujita, K., Sato, S., and Abe T., "Experimental Study of Nonequilibrium Phenomena behind Strong Shock Waves Generated in Super-orbital Reentry Flight," AIAA Paper, AIAA2002-3101, 8th AIAA/ASME Joint Thermophysics and Heat Transfer Conference, St. Lois, MO, June (2002).
  6. Kazuhisa Fujita, Shunichi Sato, Takashi Abe and Yuta Ebinuma, "Experimental Investigation of Air Radiation from behind a Strong Shock Wave, " Journal of Thermophysics and Heat Transfer, Vol.16, No.1, p.77-82, (2002).


<2001年度>

  1. Kazuhisa Fujita, Shunichi Sato, Takashi Abe and Atsushi Matsuda, "Electron Temperature and Density Measurement ahead of Strong Shock Waves, " 35th AIAA Thermophysics Conference : Anaheim, CA: AIAA Paper, AIAA2001-2765, June (2001).
  2. Hirotaka Otsu, Norihiko Kanai, Kazuhisa Fujita and Takashi Abe, "Effect of Models for Transport Properties on the Hypersonic Reentry Heating Environment, " 35th AIAA Thermophysics Conference : Anaheim, CA : AIAA Paper, AIAA2001-2831, June, (2001).
  3. Atsushi Matsuda, Shunichi Sato, Kazuhisa Fujita and Takashi Abe, "Experimental Study for the Shock Layer Generated in a Super-orbital Reentry Flight, " Proceedings of the 23rd International Symposium on Shock Waves, (to be published): (2001).
  4. Akihiro Sasoh, Yasuyuki Ohnishi, Djameel Ramjaun, Kazuyoshi Takayama, Hirotaka Otsu and Takashi Abe, "Effectiv Test Time Evaluation in High Enthalpy Tube, " AIAA Journal : Vol.39, No.11, p.2141-2147, (2001).
  5. Takashi Abe, Kazuhisa Fujita and Hirotaka Otsu, "Reentry Environment Advanced Diagnostics (READ) flight experiment on USERS reentry vehicle, " AIAA/NAL-NASDA-ISAS 10th International Space Planes and Hypersonic Systems and Technologies Conference, Kyoto : Japan : AIAA Paper2001-1051, (2001).


<2000年度>

  1. Fujita, K and Abe, T, "Assessment of Rotational Nonequilibrium Impact on the Aerodynamic Heating Rate," AIAA Paper, AIAA2000-2588, AIAA 34th Thermophysics Conference, at Denver, USA, (2000).
  2. Abe, T., Sato, S., Yamamoto, K. and Matsukawa, Y, "Experimental Investigation of Dynamically Unstable Motion of Reentry Capsule," AIAA Paper, AIAA2000-2589, AIAA 34th Thermophysics Conference, at Denver USA, (2000).
  3. Abe, T., Fujita, K., Ogawa, H. and Funaki, I.. "Microwave Telementry Breakdown Caused by Rocket Plumes," AIAA Paper, AIAA2000-2484, AIAA 34th Thermophysics Conference, at Denver, USA, (2000).
  4. Fujita, K., Matsuda, A., Sato, S. and Abe, T. "Precursor Electron Density Measurement ahead of Strong Shock Waves," RGD-13007, Proceedings of the 22nd International Symposium on Rarefied Gas Dynamics, at Australia, (2000).
  5. Hirotani, T., Sato, S., Yamamoto, Y., Suzuki, K. and Abe, T. "Spacecraft Contamination by Propulsion Jet Impinging on Dusty Planetary Surface," RGD-9015, Proceedings of the 22nd International Symposium on Rarefied Gas Dynamics, Sydney, Australia, (2000).
  6. Y. Morita, J. Kawaguchi, Y. Inatani, T. Abe, "Development status of the high-speed reentry system---DASH," IAF-00-V.2.02, 51st International Astronautical Congress, 2-6 Oct 2000, at Rio de Janeiro, Brazil, (2000).
  7. T. Abe, Y. Morita, J. Kawaguchi, Y. Inatani, "Development status of the high-speed reentry system---DASH," 2nd International Symposium Atmospheric Reentry Vehicles and Systems, at Arcachon, France, (2000).
  8. T. Abe, K. Fujita, H. Ogawa and I. Funaki, "Microwave Telementry Breakdown Caused by Rocket Plume," Proc. of the Third Asian-Pacific Conference on Aerospace Technology and Science, at Kunming, China, Oct.4-8, (2000).


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