A.【査読付き学術誌】研究業績

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

1. Susumu HASEGAWA, Masaaki FUKUI, Yoshimasa NISHIMURA, and Kazuhide MIZOBATA,
   Flow Analysis around Spaceplane for Airframe Engine Integration by CFD,
   Transaction of JSASS, Aerospace Technology Japan, 2021, Volume 19, Issue 4, Pages 577-583, DOI https://doi.org/10.2322/tastj.19.577
2. G. Coral, K. Kinefuchi, D. Nakata, R. Tsukizaki, K. Nishiyama, H. Kuninaka,
   Design and testing of additively manufactured high-efficiency resistojet on hydrogen propellant,
   Acta Astronautica 2021, doi: https://doi.org/10.1016/j.actaastro.2020.12.047. Accepted on 24th, Dec. 2020. Published online Volume 181, April 2021, Pages 14-27
3. Daisuke Nakata, Kiyoshi Kinefuchi, Hitoshi Sakai and Suyalatu,
   Thermal Design and Experimental Verification of a 3D-Printed Resistojet,
   Journal of Propulsion and Power, Accepted on 25th June, 2021 Published Online:6 Sep 2021, https://doi.org/10.2514/1.B38187, Published Paper: Journal of Propulsion and Power 2022 Vol.38 No.1, pp.148–156
4. Koichi Inoue, Haruhiko Ohta, Hitoshi Asano, Osamu Kawanami, Ryoji Imai, Koichi Suzuki, Yasuhisa Shinmoto, Takashi Kurimoto, Satoshi Matsumoto,
   Heat Loss Analysis of Flow Boiling Experiments Onboard International Space Station with Unclear Thermal Environmental Conditions (2nd Report: Liquid-vapor Two-phase Flow Conditions at Test Section Inlet),
   Microgravity Science and Technology, 2021, https://doi.org/10.1007/s12217-021-09902-7.
5. Masazumi UEBA,Tomohiro KAMATA Sakurako NAKAJIMA, and Yosuke MAEDA,
   Verification of Fully Autonomous Flight from Takeoff to Landing of a Low-SpeedModel Airplane with Application to a Small Unmanned Supersonic Airplane,
   Trans. JSASS Aerospace Tech. Japan, Vol.19, No.5, pp.667-675, 2021, DOI: 10.2322/tastj.19.667
6. Kiyoshi Kinefuchi, Daisuke Nakata, Giulio Coral, Suyalatu, Hitoshi Sakai, Tsukizaki Ryudo and Kazutaka Nishiyama,
   Additive-manufactured single-piece thin malti-layer tungsten heater for an electrothermal thruster,
   Review of Scientific Instruments, Vol.92, Issue 11, published online 9thNov., 2021, https://doi.org/10.1063/5.0068926
7. Yasuda K, Nakata D. and Uchiumi M.,
   Experimental Study on Temperature Change by Cavitation accompanying Self-pressurization of Propellant for Small Rocket Engines,
   ASME, J. Fluids Eng.Vol.143(12) 121103(2021).
8. Naoki SOTA, Ryoji IMAI, Aoki ANADA, Taisei YAMAZAKI, Masaharu UCHIUMII,Daisuke NAKATA, and Ryojiro MINATO,
   Study on Propellant Supply System for a Small-scale Supersonic Flight Experiment Vehicle (Study on a Propellant Management Device),
   Int. J.Microgravity Sci. Appl.，Vol.38, No.1, 2021, https://doi.org/10.15011/jasma.39.390103.
9. Valentin Buyakofu, Ken Matsuoka, Koichi Matsuyama, Akira Kawasaki, Hiroaki Watanabe, Noboru Itouyama, Keisuke Goto, Kazuki Ishihara, Tomoyuki Noda, and Jiro Kasahara, Akiko Matsuo, Ikkoh Funaki, Daisuke Nakata, Masaharu Uchiumi, Hiroto Habu, Shinsuke Takeuchi, Satoshi Arakawa, Junichi Masuda and Kenji Maehara
   Development of an S-Shaped Pulse Detonation Engine for a Sounding Rocket,
   Journal of Spacecrafts and Rockets, Accepted on Oct. 25, 2021.
10. 中村慎太郎, 荒木幹也, ゴンザレスファン, 山岸晃己, 安田一貴, 中田大将, 内海政春,
    ハイブリッドロケットの音響放射特性,
    日本航空宇宙学会, Accepted on 27th, Jan. 2022
11. Valentin Buyakofu, Ken Matsuoka, Koichi Matsuyama, Akira Kawasaki, Hiroaki Watanabe, Noboru Itouyama, Keisuke Goto, Kazuki Ishihara, Tomoyuki Noda, Jiro Kasahara, Akiko Matsuo, Ikkoh Funaki, Daisuke Nakata, Masaharu Uchiumi, Hiroto Habu, Shinsuke Takeuchi, Satoshi Arakawa, Junichi Masuda, Kenji Maehara, Tatsuro Nakao, Kazuhiko Yamada,
    Flight Demonstration of Pulse Detonation Engine Using Sounding Rocket S-520-31,
    submitted on Jan. 2022
12. Keisuke Goto, Ken Matsuoka, Koichi Matsuyama, Akira Kawasaki, Hiroaki Watanabe, Noboru Itouyama, Kazuki Ishihara, Valentin Buyakofu, Tomoyuki Noda, Jiro Kasahara, Akiko Matsuo, Ikkoh Funaki, Daisuke Nakata, Masaharu Uchiumi, Hiroto Habu, Shinsuke Takeuchi, Satoshi Arakawa, Junichi Masuda, Kenji Maehara, Tatsuro Nakao, Kazuhiko Yamada,
    Space Flight Demonstration of Rotating Detonation Engine Using Sounding Rocket S-520-31,
    Journal of Spacecraft and Rockets, submitted on 23, Feb., 2022
13. Koki Hamajima, Kei Yasukawa, Masazumi Ueba,
    Design and evaluation of antenna pointing control system onboard fixed-wing UAV to realize video transmission relay station,
    Accepted for publication for the IEICE Communications Express (ComEX)on 19th Jan., 2022
14. Kei Yasukawa, Koki Hamajima, Masazumi Ueba,
    Turning path tracking control technology for fixed-wing UAV to realize video transmission relay station,
    Accepted for publication for the IEICE Communications Express (ComEX)on 28th Feb., 2022
15. Satoshi Hyokawa, Masazumi Ueba,
    Short-Distance Landing Control System for an 1/3-Scale Unmanned Supersonic Experimental Airplane,
    submitted to Aerospace Technology of Japan, on 4th Feb., 2022
16. Sho Shimada, Masazumi Ueba,
    Highly Accurate Flight-path Tracking Control System of the 1/3‑scale Unmanned Small Supersonic Aircraft to Realize a Flight from Take-off to Landing,
    submitted to Aerospace Technology of Japan, on 28th Feb., 2022
17. Kazuhide Mizobata, Taichi MIO, Katsuya MIYAMOTO, Yuki YAMAZAKI,
    Drag Reduction on the Basis of the Area Rule of the Small-scale Supersonic FlightExperiment Vehicle Being Developed at Muroran Institute of Technology (SecondReport),
    submitted to Transactions of JSASSon April 17, 2022.