B.【国際学会発表論文】研究業績

-------------------------2021年度-------------------------------------

1. R. Watanabe, Y. Shimizu, K. Yasuda, D. Nakata,
   Numerical Estimation of Discharge Coefficient of Nitrous Oxide Flow inside an Injector for Hybrid Rocket Engine,
   33rd International Symposium on Space Technology and Science, 2022-o-1-07, 2022.
2. A. Kawasaki, K. Matsuyama, K. Matsuoka, H. Watanabe, N. Itouyama, K. Goto, K. Ishihara, V. Buyakofu, T. Noda, J. Kasahara, A. Matsuo, I. Funaki, D. Nakata, M. Uchiumi, H. Habu, S. Takeuchi, S. Arakawa, J. Masuda, K. Maehara, T. Nakao, K. Yamada,
   In-Space Flight Demonstration Results of a Detonation Engine System on Sounding Rocket S-520-31: System Design,
   33rd International Symposium on Space Technology and Science, Beppu, Oita, February 26th-March 2nd, 2022.
3. H. Watanabe, K. Matsuyama, K. Matsuoka, A. Kawasaki, N. Itouyama, K. Goto, K. Ishihara, V. Buyakofu, T. Noda, S. Ito, J. Kasahara, A. Matsuo, I. Funaki, D. Nakata, M. Uchiumi, H. Habu, S. Takeuchi, S. Arakawa, J. Masuda, K. Maehara, T. Nakao, K. Yamada,
   In-Space Flight Demonstration Results of a Detonation Engine System on Sounding Rocket S-520-31: Flight Path and Attitude,
   33rd International Symposium on Space Technology and Science, Beppu, Oita, February 26th-March 2nd, 2022.
4. K. Goto, K. Matsuyama, K. Matsuoka, A. Kawasaki, H. Watanabe, N. Itouyama, K. Ishihara, V. Buyakofu, T. Noda, J. Kasahara, A. Matsuo, I. Funaki, D. Nakata, M. Uchiumi, H. Habu, S. Takeuchi, S. Arakawa, J. Masuda, K. Maehara, T. Nakao, K. Yamada,
   In-Space Flight Demonstration Results of a Detonation Engine System on Sounding Rocket S-520-31: Rotating Detonation Engine,
   33rd International Symposium on Space Technology and Science, Beppu, Oita, February 26th-March 2nd, 2022.
5. V. Buyakofu, K. Matsuoka, K. Matsuyama, K. Goto, A. Kawasaki, H. Watanabe, N. Itouyama, K. Ishihara, T. Noda, J. Kasahara, A Matsuo, I. Funaki, D. Nakata, M. Uchiumi, H. Habu, S. Takeuchi, S. Arakawa, J. Masuda, K. Maehara, Y. Kazuhiko, T. Nakao,
   In-Space Flight Demonstration Results of a Detonation Engine System on Sounding Rocket S-520-31: Pulse Detonation Engine,
   33rd International Symposium on Space Technology and Science, Beppu, Oita, February 26th-March 2nd, 2022.
6. A. Kawasaki, K. Matsuyama, K. Matsuoka, H. Watanabe, N. Itouyama, K. Goto, K. Ishihara, V. Buyakofu., T. Noda, J. Kasahara, A. Matsuo, F. Funaki, D. Nakata, M. Uchiumi, H. Habu, S. Takeuchi, S. Arakawa, J. Masuda, K. Maehara, T. Nakao, K. Yamada,
   Flight Demonstration of Detonation Engine System Using Sounding Rocket S-520-31: System Design,
   AIAA SciTech 2022, AIAA-2022-0229, San Diego, CA ＆ Online, January 3-7, 2022.
7. N. Itouyama, K. Matsuyama, K. Matsuoka, A. Kawasaki, H. Watanabe, K. Goto, K. Ishihara, V. Buyakofu, T. Noda, J. Kasahara, A. Matsuo, I. Funaki, D. Nakata, M. Uchiumi, H. Habu, S. Takeuchi, S. Arakawa, J. Masuda, K. Maehara, T. Nakao, K. Yamada,
   Flight Demonstration of Detonation Engine System Using Sounding Rocket S-520-31: History from Development to Flight,
   AIAA SciTech 2022, AIAA-2022-0230, San Diego, CA ＆ Online, January 3-7, 2022.
8. H. Watanabe, K. Matsuyama, K. Matsuoka, A. Kawasaki, N. Itouyama, K. Goto, K. Ishihara, V. Buyakofu, T. Noda, S. Ito, J. Kasahara, A. Matsuo, I. Funaki, D. Nakata, M. Uchiumi, H. Habu, S. Takeuchi, S. Arakawa, J. Masuda, K. Maehara, T. Nakao, K. Yamada,
   Flight Demonstration of Detonation Engine System Using Sounding Rocket S-520-31: Flight Path and Attitude,
   AIAA SciTech 2022, AIAA-2022-0231, San Diego, CA ＆ Online, January 3-7, 2022.
9. K. Goto, K. Matsuoka, K. Matsuyama, A. Kawasaki, H. Watanabe, N. Itouyama, K. Ishihara, V. Buyakofu, T. Noda, J. Kasahara, A. Matsuo, I. Funaki, D. Nakata, M. Uchiumi, H. Habu, S. Takeuchi, S. Arakawa, J. Masuda, K. Maehara, T. Nakao, K. Yamada,
   Flight Demonstration of Detonation Engine System Using Sounding Rocket S-520-31: Performance of Rotating Detonation Engine,
   AIAA SciTech 2022, AIAA-2022-0232, San Diego, CA ＆ Online, January 3-7, 2022.
10. V. Buyakofu, K. Matsuoka, K. Matsuyama, K. Goto, A. Kawasaki, H. Watanabe, N. Itouyama, K. Ishihara, T. Noda, J. Kasahara, A. Matsuo, I. Funaki, D. Nakata, M. Uchiumi, H. Habu, S. Takeuchi, S. Arakawa, J. Masuda, K. Maehara, T. Nakao, K. Yamada,
    Flight Demonstration of Detonation Engine System Using Sounding Rocket S-520-31: Performance of Pulse Detonation Engine, AIAA Scitech2022, AIAA-2022-0233, San Diego, CA ＆ Online, January 3-7,2022.
11. Kazuki Yasuda, Tatsuhiko Shiina, Daisuke Nakata, Masaharu Uchiumi,
    Experimental Study on Filling and Discharging Characteristics of Nitrous Oxide to Spacecraft Tanks, 33rd International Symposium on Space Technology and Science, Beppu, Oita, February 26th-March 2nd, 2022. 022-o-1-18
12. Shintaro Nakamura, Mikiya Araki, Juan C. González Palencia, Koki Yamagishi, Kazuki Yasuda, Daisuke Nakata, Masaharu Uchiumi,
    Experimental Investigation of Hybrid Rocket Acoustics,
    33rd International Symposium on Space Technology and Science, Beppu, Oita, February 26th-March 2nd, 2022. 2022-a-39s
13. Ayano Yoshida, Ryo Ikemoto, Kazuki Shibutani, Kentaro Kaji, Hirokazu Tahara, Ai Momozawa, Daisuke Nakata, Tomoyuki Ikeda, Yoshiyuki Takao, Takashi Wakizono, Masaya Toyama,
    Performance Characteristics of High-Thrust High-specific-Impulse Steady-State Magneto-Plasma-Dynamic Thrusters for Transportation in the Solar System -Use of Carbon Dioxide, Methane, Ammonia, Hydrogen, Helium, Air and Water/Ice etc. in the Planets and Satellites to Propellants,
    33rd International Symposium on Space Technology and Science, Beppu, Oita, February 26th-March 2nd, 2022. 2022-b-22
14. Kentaro Kaji, Kazuki Shibutani, Ryo Ikemoto, Ayano Yoshida, Hirokazu Tahara, Ai Momozawa, Daisuke Nakata, Tomoyuki Ikeda, Yoshiyuki Takao, Yuichiro Nogawa, Takashi Wakizono, Masaya Toyama,
    Performance Characteristics of DC Arcjet Thrusters -Use of Carbon Dioxide, Methane, Ammonia, Hydrogen, Helium, Air and Water/Ice etc. in Planets and Satellites in the Solar System to Propellants,
    33rd International Symposium on Space Technology and Science, Beppu, Oita, February 26th-March 2nd, 2022. 2022-b-21
15. Daisuke Nakata, Kazuki Yasuda, Akihiro Watanabe, Ang YiYong, Koki Yamagishi, Tatsuhiko Shiina, Takuya Tada, Iori Obara, Yuma Hashimoto, Hikaru Eguchi, Masaharu Uchiumi,
    Rocket Sled System Design for Various Missions,
    33rd International Symposium on Space Technology and Science, Beppu, Oita, February 26th-March 2nd, 2022, 2022-o-1-05
16. Shuuta Haraguchi, Shun Sasaki, Atsuya Honda, Akihiro Nishida, Ryuto Kawanabe, Haruka Nikado, Kazuhide Mizobata,
    Flowfield Visualization and Mechanism of Dynamic Derivatives of a Small-scale Supersonic Flight Experiment Vehicle Being Developed at Muroran Institute of Technology,
    33rd International Symposium on Space Technology and Science, online, February 26th-March 2nd, 2022, 2022-g-03.
17. Tomohiro SHIGEKIYO, Nana HASEGAWA, Katsuya MIYAMOTO, and Kazuhide MIZOBATA,
    Drag Reduction of the Small-scale Supersonic Flight Experiment Vehicle Being Developed at Muroran Institute of Technology (Third Report),
    33rd International Symposium on Space Technology and Science, online, February 26th-March 2nd, 2022, 2022-g-04.