Presentaion at conference, meeting, etc. - MIZOBATA Kazuhide

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  1. A Reusable Hybrid RocketSystem: Concept Outlines and Feasibility of Winged Flights

    Mizobata, K., Nagata, H., Itoh, K., Akiba, R. and Kubota, I.,22nd International Symposium on Space Technology and Science,Japan Society for Aeronautical and Space Sciences,22nd International Symposium on Space Technology and Science,2000.10,Morioka, Japan,Japan

  2. An Approach for Teaching Aircraft Propulsion Systems using a Micro Turbojet Engine for Undergraduate Laboratory Course Students in Japanese University

    T. Arai, J. Kasahara, K. Mizobata, H. Sugiyama, Y. Hanaoka, H. Hoya, and Y. Nishi,8th International Symposium on Transport Phenomena and Dynamics of Rotating Machinery (ISROMAC-8),8th International Symposium on Transport Phenomena and Dynamics of Rotating Machinery (ISROMAC-8),2000.03,Honolulu, Hawaii, USA,United States

  3. Conceptual Feasibility of Reusable Launch Vehicles Based on the ATREX Engine

    K. Mizobata, T. Arai, and H. Sugiyama,AIAA 9th International Space Planes and Hypersonic Systems and Technologies Conference,American Institute of Aeronautics and Astronautics,AIAA 9th International Space Planes and Hypersonic Systems and Technologies Conference,1999.11,Norfolk, USA,United States

  4. Shock Propagation and Bubble Collapse in Two-Phase Fluids

    H. Sugiyama, K. Ohtani, K. Mizobata, T. Arai,3rd ASME/JSME Joint Fluids Engineering Conference,American Society of Mechanical Engineers,3rd ASME/JSME Joint Fluids Engineering Conference,1999.07,San Francisco, USA,United States

  5. An Analysis of Rotational Rate Processes in Expanding Flows in Nitrogen

    K. Mizobata, C. Park, and S. Ogawa,Colloquium on Nonequilibrium Phenomena of Low-Density Jets in Space,Colloquium on Nonequilibrium Phenomena of Low-Density Jets in Space,1998.02,Kyoto, Japan,Japan

  6. Conceptual Design of the LE-7-based Reusable Launch Systems

    M. Nakajima, K. Mizobata, and K. Sawada,36th Aerospace Sciences Meeting,American Institute of Aeronautics and Astronautics,36th Aerospace Sciences Meeting,1998.01,Reno, NV, USA,United States

  7. An Analysis of Rotational Rate Processes in Expanding Flows in Nitrogen

    K. Mizobata, C. Park, and S. Ogawa,36th Aerospace Sciences Meeting,American Institute of Aeronautics and Astronautics,36th Aerospace Sciences Meeting,1998.01,Reno, NV, USA,United States

  8. An Analysis of Quasiclassical Molecular Collision and Rate Processes for Coupled Vibration-Dissociation and Recombination

    Kazuhide MIZOBATA,35th Aerospace Sciences Meeting,American Institute of Aeronautics and Astronautics,35th Aerospace Sciences Meeting,1997.01,Reno, NV, USA,United States

  9. Conceptual Study of an Airbreathing Reusable Launch Vehicle

    S. Takahashi, K. Mizobata, and K. Sawada,35th Aerospace Sciences Meeting,American Institute of Aeronautics and Astronautics,35th Aerospace Sciences Meeting,1997.01,Reno, NV, USA,United States

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