Rchr
J-GLOBAL ID:200901080238072150   Update date: Oct. 02, 2019

NAGATA Harunori

ナガタ ハルノリ | NAGATA Harunori
Affiliation and department:
Job title: Professor
Homepage URL  (2): http://mech-me.eng.hokudai.ac.jp/~spacesystem/http://mech-me.eng.hokudai.ac.jp/~spacesystem/
Research field  (2): Thermal engineering ,  Aerospace engineering
Research keywords  (4): Space Propulsion ,  Microgravity Engineering ,  Combustion ,  Space Propulsion
Research theme for competitive and other funds  (7):
  • 2006 - 2008 Regression Mechanism of a Solid Fuel around Oxidizer Jet Stagnation Region
  • 2001 - 2002 Shock Induced Combustion and Flame Folding in Supersonic Combustion Ramjet Engine
  • 2000 - 2002 Development Study of High-response Hydrogen Concentration Probe for Supersonic Flows
  • 1999 - 2000 SUPERSONIC MIXING AND COMBUSTION OF HYDROGEN USING HIGH-ENTHALPY SHOCK TUNNEL
  • 1998 - 2000 Generation and Collection of Droplets under microgravity
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Papers (68):
  • Gotoh Ryohei, Totani Tsuyoshi, Wakita Masashi, Nagata Harunori. Controlling heat release of crystallization from supercooling state of a solid-solid PCM, 2-amino-2-methyl-1,3-propanediol. INTERNATIONAL JOURNAL OF HEAT AND MASS TRANSFER. 2019. 137. 1132-1140
  • Kamps Landon, Sakurai Kazuhito, Saito Yuji, Nagata Harunori. Comprehensive Data Reduction for N2O/HDPE Hybrid Rocket Motor Performance Evaluation. AEROSPACE. 2019. 6. 4
  • Saito Yuji, Kimino Masaya, Tsuji Ayumu, Okutani Yushi, Soeda Kentaro, Nagata Harunori. High Pressure Fuel Regression Characteristics of Axial-Injection End-Burning Hybrid Rockets. JOURNAL OF PROPULSION AND POWER. 2019. 35. 2. 328-341
  • Ezoe Yuichiro, Miyoshi Yoshizumi, Kasahara Satoshi, Kimura Tomoki, Ishikawa Kumi, Fujimoto Masaki, Mitsuda Kazuhisa, Sahara Hironori, Isobe Naoki, Nakajima Hiroshi, Ohashi Takaya, Nagata Harunori, Funase Ryu, Ueno Munetaka, Branduardi-Raymont Graziella. Ultralightweight x-ray telescope missions: ORBIS and GEO-X. JOURNAL OF ASTRONOMICAL TELESCOPES INSTRUMENTS AND SYSTEMS. 2018. 4. 4
  • Mitchao Delburg P., Totani Tsuyoshi, Wakita Masashi, Nagata Harunori. Preliminary Thermal Design for Microsatellites Deployed from International Space Station's Kibo Module. JOURNAL OF THERMOPHYSICS AND HEAT TRANSFER. 2018. 32. 3. 789-798
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MISC (170):
  • Landon Kamps, Shota Hirai, Kazuhito Sakurai, Tor Viscor, Yuji Saito, Raymond Guan, Hikaru Isochi, Naoto Adachi, Mitsunori Itoh, Harunori Nagata. Investigation of graphite nozzle erosion in hybrid rockets using o2/c2h4. 2018 Joint Propulsion Conference. 2018
  • Yushi Okutani, Yuji Saito, Masaya Kimino, Ayumu Tsuji, Kentaro Soeda, Harunori Nagata. Investigation of regression rate under high-pressure in axial-injection end-burning hybrid rockets. 2018 Joint Propulsion Conference. 2018
  • Yuji Saito, Landon Kamps, Kodai Komizu, Kentaro Soeda, Daniele Bianchi, Francesco Nasuti, Harunori Nagata. The accuracy of reconstruction techniques for determining hybrid rocket fuel regression rate. 2018 Joint Propulsion Conference. 2018
  • Ryohei Gotoh, Tsuyoshi Totani, Masashi Wakita, Harunori Nagata. Control of heat release energy during heating from solid-solid phase change material. International Heat Transfer Conference. 2018. 2018-August. 4425-4432
  • Erika Uchiyama, Yurika Kiyotani, Landon Kamps, Harunori Nagata. Experimental investigation of c* efficiency in nitrous oxide hybrid rockets. Advances in the Astronautical Sciences. 2018. 166. 109-115
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Lectures and oral presentations  (24):
  • 大口径パルスデトネーションエンジン用イニシエータにおける円筒デトネーション波の伝播に関する研究
    (流体力学講演会/航空宇宙数値シミュレーション技術シンポジウム講演集(CD-ROM) 2012)
  • 固体表面上燃え拡がりの吹き飛び限界に及ぼす流路断面形状の影響
    (燃焼シンポジウム講演論文集 2012)
  • 固体燃料管内燃え拡がりにおける固相への熱輸送と消炎現象の関係
    (日本伝熱シンポジウム講演論文集(CD-ROM) 2012)
  • 金属膜を付与した表面微細周期構造の垂直放射率特性
    (日本伝熱シンポジウム講演論文集(CD-ROM) 2012)
  • サブオービタル機開発に向けての飛行実験と今後の計画
    (飛行機シンポジウム講演集(CD-ROM) 2012)
more...
Work history (1):
  • 1994 - 1996 Technical Staff,Aerospace Div., Nissan Motor Co., Ltd.
Awards (9):
  • 2019/08 - The American Institute of Aeronautics and Astronautics 2018 AIAA Hybrid Rockets Best Paper Award Investigation of Graphite Nozzle Erosion in Hybrid Rockets Using O2/C2H4
  • 2018/04 - Fellow member
  • 2017/07 - The American Institute of Aeronautics and Astronautics 2016 Hybrid Rockets Student Best Paper Award Experimental and Analytical Investigation of Effect of Pressure on Regression Rate of Axial-Injection End-Burning Hybrid Rockets
  • 2013/03 - Fellow member
  • 2008 - Japan Society for Aeronautics and Space Sciences JSASS Award
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