宇宙システム工学

研究成果

年別の研究成果 1982 2004 2005 2006 2008 2009 2010 2011 2013 2014 2015 2016 2017 2020 2021 2022 2024 2025

• 193 会議への寄与
• 166 学術誌
• 43 学会誌
• 41 会議記事
• 18 その他
  • 6 章
  • 3 コメント/討論
  • 3 編集
  • 3 総説
  • 2 章 (査読審査付き)
  • 1 前書き/後書き

年別の研究成果

年別の研究成果

検索結果

• 2014

  Improvement of nucleate boiling heat transfer characteristics by using immiscible mixtures

  Kita, S., Onishi, S., Fukuyama, Y. & Ohta, H., 1月 1 2014.

  研究成果: 会議への寄与タイプ › 学会誌 › 査読

  • Liquids 100%
  • Surface Temperature 66%
  • Nucleate Boiling 66%
  • Heat Transfer 66%
  • Reduction 50%
  2 被引用数 (Scopus)
• 2012

  Experimental study of the morphing flap as a low noise high lift device for aircraft wing

  Tani, Y., Matsuda, Y., Doi, A., Yamashita, Y., Aso, S. & Ito, T., 2012, p. 1042-1048. 7 p.

  研究成果: 会議への寄与タイプ › 学会誌 › 査読

  • Flaps 100%
  • Wings 44%
  • Deflection 22%
  • Lift Device 22%
  • Flap Configuration 22%
  1 被引用数 (Scopus)

• Supersonic flight separation simulation for TSTO launch vehicles considering shock wave interaction reduction

  Uematsu, T., Aso, S. & Tani, Y., 2012.

  研究成果: 会議への寄与タイプ › 学会誌 › 査読

  • Increasing 100%
  • Simulation 66%
  • Cross Sections 66%
  • Interference 66%
  • Shock Wave 66%
  9 被引用数 (Scopus)
• 2005

  A new thermal protection system by opposing jet for reusable launch vehicles

  Hayashi, K., Aso, S. & Tani, Y., 2005, p. 5322-5332. 11 p.

  研究成果: 会議への寄与タイプ › 学会誌 › 査読

  • Model 100%
  • Flow Distribution 100%
  • Supersonic Flow 100%
  • Protection System 100%
  • Models 100%
  1 被引用数 (Scopus)

• Applying a simple contol law to deploy space tether on a micro Tethered satellite

  Tanaka, Y., Hanada, T. & Hirayama, H., 2005, p. 2337-2344. 8 p.

  研究成果: 会議への寄与タイプ › 学会誌

  • Satellites 100%
  • Deployment 83%
  • Tethered Satellite 50%
  • Project 33%
  • University 33%
  1 被引用数 (Scopus)

• Are de-orbiting missions possible using electrodynamic tethers? Task review from the space debris perspective

  Pardini, C., Hanada, T., Krisko, P. H., Luciano Anselmo, I. & Hirayama, H., 2005, p. 2554-2566. 13 p.

  研究成果: 会議への寄与タイプ › 学会誌 › 査読

  • Debris 100%
  • Orbitals 60%
  • Meteoroids 60%
  • Diameters 40%
  • Impact 40%
  2 被引用数 (Scopus)

• A study on the enhancement of supersonic mixing by using RMP shaped injector with shock generator and cavity

  Inoue, K., Yamaguchi, K., Aso, S. & Tani, Y., 2005, p. 4643-4649. 7 p.

  研究成果: 会議への寄与タイプ › 学会誌 › 査読

  • Injector 100%
  • Supersonics 55%
  • Pressure 33%
  • Temperature 22%
  • Gases 22%

• Characterizing fragments from impact on a micro satellite

  Nakashima, K., Hanada, T., Harano, T., Machida, Y., Koura, T. & Akahoshi, Y., 2005, p. 2527-2534. 8 p.

  研究成果: 会議への寄与タイプ › 学会誌 › 査読

  • Model 100%
  • Collision 100%
  • Models 100%
  • Standard 83%
  • Low Speed 66%

• Feasibility study on the thermal management system for space solar power system

  Ohta, H., Ando, M. & Shinmoto, Y., 2005, p. 4153-4162. 10 p.

  研究成果: 会議への寄与タイプ › 学会誌 › 査読

  • Cooling 100%
  • Loop 66%
  • Transportation 66%
  • Feasibility 66%
  • Laser 66%
  1 被引用数 (Scopus)

• Improvement of aerodynamic performances for reusable launch vehicles using the lateral blowing

  Tadakuma, K., Aso, S. & Tani, Y., 2005, p. 5270-5279. 10 p.

  研究成果: 会議への寄与タイプ › 学会誌 › 査読

  • Wings 100%
  • Aerodynamic Characteristic 100%
  • Reusable Launch Vehicle 75%
  • Reusable Launch Vehicles 75%
  • Supersonic Flow 50%
  1 被引用数 (Scopus)

• Jovian outpost establishment trajectory design

  Poetro, R. E., Yasaka, T., Hanada, T. & Hirayama, H., 2005, p. 720-726. 7 p.

  研究成果: 会議への寄与タイプ › 学会誌 › 査読

  • Gravitation 100%
  • Exploration 50%
  • Solar System 50%
  • Natural Resources Exploration 50%
  • Trajectories 50%

• Low energy frequent Europa - Callisto trajectories

  Poetro, R. E., Yasaka, T., Hanada, T. & Hirayama, H., 2005, p. 6241-6246. 6 p.

  研究成果: 会議への寄与タイプ › 学会誌 › 査読

  • Callisto 100%
  • Europa 100%
  • Energy Engineering 100%
  • Trajectories 100%
  • Transportation 66%

• Numerical study of thermal protection system by opposing jet

  Hayashi, K., Aso, S. & Tani, Y., 2005, p. 11641-11648. 8 p.

  研究成果: 会議への寄与タイプ › 学会誌 › 査読

  • Reduction 100%
  • Aerodynamic Heating 80%
  • Supersonic Flow 80%
  • Model 40%
  • Region 40%
  84 被引用数 (Scopus)

• Searching the lost fragments

  Ikeda, H., Hanada, T. & Yasaka, T., 2005, p. 2682-2687. 6 p.

  研究成果: 会議への寄与タイプ › 学会誌 › 査読

  • Explosion 100%
  • Debris 66%
  • Attraction 66%
  • Model 33%
  • Particle 33%

• Stochastic analysis of survivability of double tether

  Hirayama, H., Oishi, A., Hanada, T. & Yasaka, T., 2005, p. 2688-2692. 5 p.

  研究成果: 会議への寄与タイプ › 学会誌 › 査読

  • Survivability 100%
  • Space Debris 60%
  • Collisions 40%
  • Model 20%
  • Estimates 20%
• 2004

  A consideration on size and area-to-mass distributions for breakup fragments

  Hata, H., Hanada, T., Yasaka, T., Akahoshi, Y. & Harada, S., 2004, p. 3808-3816. 9 p.

  研究成果: 会議への寄与タイプ › 学会誌 › 査読

  • Model 100%
  • Area 100%
  • Mass Distribution 100%
  • Models 100%
  • Collisions 80%
  1 被引用数 (Scopus)

• Assessment of collision risk to electrodynamic tether used for de-orbiting

  Oishi, A., Hirayama, H., Hanada, T., Yasaka, T., Pardini, C. & Anselmo, L., 2004, p. 4065-4071. 7 p.

  研究成果: 会議への寄与タイプ › 学会誌 › 査読

  • Collision Risk 100%
  • Debris 75%
  • Electrodynamics 75%
  • Orbitals 75%
  • Collision 75%
  6 被引用数 (Scopus)

• A study on increase of duration of a free piston shock tunnel

  Mizoguchi, M., Aso, S., Futae, S. & Hayashi, K., 2004, p. 10459-10468. 10 p.

  研究成果: 会議への寄与タイプ › 学会誌 › 査読

  • Piston 100%
  • Diaphragm 66%
  • Convergent 50%
  • Shock Tunnels 50%
  • Experimental Result 33%
  1 被引用数 (Scopus)

• Fundamental study of supersonic combustion in pure air flow with use of shock tunnel

  Aso, S., Hakim, A. N., Miyamoto, S., Inoue, K. & Tani, Y., 2004, p. 7166-7171. 6 p.

  研究成果: 会議への寄与タイプ › 学会誌 › 査読

  • Region 100%
  • Combustion 100%
  • Shock Tunnels 100%
  • Supersonic Combustion 100%
  • Pressure 50%

• Kyushu university micro-satellite qtex project

  Kuwahara, T., Yasaka, T., Hanada, T., Hirayama, H., Sakamoto, Y. & Itahashi, T., 2004, p. 3604-3612. 9 p.

  研究成果: 会議への寄与タイプ › 学会誌 › 査読

  • Satellites 100%
  • Public Relations 55%
  • Universities 33%
  • Bus 33%
  • Deployment 33%
  6 被引用数 (Scopus)

• Low-velocity projectile impacts on solar arrays

  Kawamura, T., Hirayama, H., Kanada, T. & Yasaka, T., 2004, p. 2115-2121. 7 p.

  研究成果: 会議への寄与タイプ › 学会誌 › 査読

  • Impact 100%
  • Low Speed 66%
  • Spacecraft 50%
  • Size 33%
  • Calibration 33%
  1 被引用数 (Scopus)
• 2003

  A study on fundamental aerodynamic characteristics of future space transportation systems

  Yoneda, T., Aso, S., Tsuchiya, S. & Morita, W., 2003, p. 1985-1993. 9 p.

  研究成果: 会議への寄与タイプ › 学会誌 › 査読

  • Wings 100%
  • Reusable Launch Vehicle 66%
  • Body Model 66%
  • Max 50%
  • Lifting Body 50%
  7 被引用数 (Scopus)

• A study on the effect of fuel injection angle to two-dimensional supersonic mixing for SCRAM-jet engine and PDE

  Inoue, K., Aso, S. & Kawano, S., 2003, p. 475-483. 9 p.

  研究成果: 会議への寄与タイプ › 学会誌 › 査読

  • Supersonics 100%
  • Injection 100%
  • Flow Distribution 75%
  • Flat Plates 75%
  • Experiments 75%
  3 被引用数 (Scopus)

• Importance of seminar of science volunteers for attractive space education for youngsters

  Aso, S., Matogawa, Y., Miyazaki, S. & Fukuda, K., 2003, p. 3161-3164. 4 p.

  研究成果: 会議への寄与タイプ › 学会誌 › 査読

  • Education 100%
  • Science 100%
  • Volunteers 100%
  • Fellowships 14%
  • Japan 14%

• In-situ debris measurements in GEO through optical surface inspection

  Hirayama, H., Hanada, T. & Yasaka, T., 2003, p. 1647-1652. 6 p.

  研究成果: 会議への寄与タイプ › 学会誌 › 査読

  • Measurement 100%
  • Inspection 100%
  • Situ Measurement 100%
  • Optical Surface 100%
  • In Situ 100%

• In-situ debris measurements in GEO through optical surface inspection

  Hirayama, H., Hanada, T. & Yasaka, T., 2003, p. 3551-3556. 6 p.

  研究成果: 会議への寄与タイプ › 学会誌 › 査読

  • Debris 100%
  • Space Debris 100%
  • In Situ Measurement 75%
  • in Situ Measurement 75%
  • Surfaces 50%
  2 被引用数 (Scopus)

• Modifying the NASA standard breakup model to be applied to low-velocity collision

  Hata, H., Akahoshi, Y., Harada, S., Kurakazu, Y., Hanada, T. & Yasaka, T., 2003, p. 1309-1318. 10 p.

  研究成果: 会議への寄与タイプ › 学会誌 › 査読

  • Low Speed 100%
  • Low Velocity 100%
  • Model 66%
  • Experiment 66%
  • Impact 66%
  3 被引用数 (Scopus)

• On the feasibility of heat removal from generator/transmitter units for assumed 10MW space solar power system by using two-phase flow loop with latent heat transportation

  Ohta, H., Tôyama, S., Kawasaki, H., Ohno, T. & Mori, M., 2003, p. 79-87. 9 p.

  研究成果: 会議への寄与タイプ › 学会誌 › 査読

  • Heat Transfer 100%
  • Generators 30%
  • Two-Phase Flow 30%
  • Latent Heat 30%
  • Satellites 30%
  5 被引用数 (Scopus)
• 2002

  Experimental and computational studies on Two-Dimensional supersonic mixing flow physics

  Aso, S., Kawano, S. & Inoue, K., 2002.

  研究成果: 会議への寄与タイプ › 学会誌 › 査読

  • Experiments 100%
  • Models 50%
  • Good Agreement 50%
  • Efficiency 50%
  • Flow Field 50%
  3 被引用数 (Scopus)
• 2000

  Active control of aerodynamic chracteristics of next-generation SST wing by lateral blowing

  Kamishita, M., Aso, S., Karashima, K. & Sato, K., 2000.

  研究成果: 会議への寄与タイプ › 学会誌 › 査読

  • Wings 100%
  • Aerodynamic Characteristic 57%
  • Low Speed 42%
  • High Speed 28%
  • Experiments 28%
  2 被引用数 (Scopus)

• A study of a new ramp injector for improvement of supersonic mixing

  Kawano, S., Aso, S. & Orino, M., 12月 1 2000.

  研究成果: 会議への寄与タイプ › 学会誌 › 査読

  • Supersonics 100%
  • Injection 100%
  • Injector 100%
  • Volume 66%
  • Gases 66%

• New code validation experiments and numerical simulations of high enthalpy flows with noneqilibrium

  Matsumoto, A., Aso, S., Suzuki, Y., Morioka, T. & Honma, H., 2000.

  研究成果: 会議への寄与タイプ › 学会誌 › 査読

  • Experiments 100%
  • Codes 75%
  • Simulation 50%
  • Computer Simulation 50%
  • Thermal Equilibrium 50%
• 1997

  A study on supersonic mixing flowfield with swept ramp injectors

  Aso, S., Yamane, Y., Umii, K., Tokunaga, K., Ando, Y. & Sakata, K., 1997.

  研究成果: 会議への寄与タイプ › 学会誌 › 査読

  • Investigation 100%
  • Supersonics 100%
  • Experiment 66%
  • Flow Structure 66%
  • Experiments 66%
  6 被引用数 (Scopus)

• Effects of dynamic stall phenomena on propulsive efficiency and thrust of a flapping airfoil

  Isogai, K., Shinmoto, Y. & Watanabe, Y., 1997.

  研究成果: 会議への寄与タイプ › 学会誌 › 査読

  • Oscillation 100%
  • Propulsive Efficiency 100%
  • Phase Difference 50%
  • Differences 50%
  • Amplitudes 50%
  1 被引用数 (Scopus)

• Experimental and computational study on reduction of aerodynamic heating load by film cooling in hypersonic flows

  Aso, S., Kurotaki, T., Miyamoto, Y., Isomura, Y., Kurosaki, R. & Katayama, M., 1997.

  研究成果: 会議への寄与タイプ › 学会誌 › 査読

  • Heat 100%
  • Protection 100%
  • Film Cooling 100%
  • Experiments 100%
  • Boundary Layer 66%
  3 被引用数 (Scopus)
• 1995

  A study on reduction of aerodynamic heating load by film cooling

  Shigeru, A. S. O., Mitomo, T., Naka, T., Nakamura, Y., Kurotaki, T., Kurosaki, R. & Katayama, M., 1995.

  研究成果: 会議への寄与タイプ › 学会誌 › 査読

  • Experiments 100%
  • Heat 100%
  • Protection 100%
  • Film Cooling 100%
  • Aerodynamic Heating 75%
  1 被引用数 (Scopus)
• 1993

  Aerodynamic heating with boundary layer transition and heat protection with mass addition on blunt body in hypersonic flows

  Aso, S., Kumamoto, Y., Kondo, N., Nakamura, Y., Katayama, M. & Kurosaki, R., 1993.

  研究成果: 会議への寄与タイプ › 学会誌 › 査読

  • Aerodynamic Heating 100%
  • Boundary Layer Transition 80%
  • Heat 60%
  • Protection 60%
  • Blunt Bodies 60%
  1 被引用数 (Scopus)

• Intensive studies on unsteady secondary separations and oscillating shock waves in three-dimensional shock waves/turbulent boundary layer interaction regions induced by sharp and blunt fins

  Aso, S., Maekawa, S., Okuyama, S., Karashima, K. & Sato, K., 1993.

  研究成果: 会議への寄与タイプ › 学会誌 › 査読

  • Shock Wave 100%
  • Interaction Region 80%
  • Turbulent Boundary Layer 80%
  • Oil 60%
  • Layer Interaction 40%
  7 被引用数 (Scopus)
• 1991

  Aerodynamic heating in three-dimensional shock wave turbulent boundary layer interaction induced by sweptback sharp fins in hypersonic flows

  Aso, S., Maekawa, S. & Hayashi, M., 12月 1 1991.

  研究成果: 会議への寄与タイプ › 学会誌 › 査読

  • Leading Edge 100%
  • Turbulent Boundary Layer 100%
  • Flow Field 75%
  • Interaction Region 75%
  • Flow Distribution 75%

• Detailed measurements on unsteady properties in three-dimensional shock wave/turbulent boundary layer interaction induced by blunt fin at Mach number 4

  Aso, S., Kuranaga, S. & Hayashi, M., 1991.

  研究成果: 会議への寄与タイプ › 学会誌 › 査読

  • Turbulent Boundary Layer 100%
  • Properties 75%
  • Interaction Region 75%
  • Pressure Fluctuation 75%
  • Shock Wave 75%
  8 被引用数 (Scopus)

• Numerical simulations of separated flows around oscillating airfoil for dynamic stall phenomena

  Aso, S., Sakamoto, A. & Hayashi, M., 12月 1 1991.

  研究成果: 会議への寄与タイプ › 学会誌 › 査読

  • Airfoil 100%
  • Experiments 75%
  • Separated Flow 75%
  • down Process 50%
  • Pitch 25%
• 1990

  Aerodynamic heating phenomena in three-dimensional shock wave/turbulent boundary layer interactions induced by sweptback blunt fins

  Aso, S., Kuranaga, S., Nakao, S. & Hayashi, M., 1990.

  研究成果: 会議への寄与タイプ › 学会誌 › 査読

  • Turbulent Boundary Layer 100%
  • Aerodynamic Heating 66%
  • Shock Wave 50%
  • Experiments 33%
  • Interaction Region 33%
  6 被引用数 (Scopus)
• 1987

  NUCLEATE BOILING HEAT TRANSFER IN VERTICAL NARROW SPACE.

  Fujita, Y., Ohta, H. & Uchida, S., 1987, p. 469-476. 8 p.

  研究成果: 会議への寄与タイプ › 学会誌 › 査読

  • Experiments 100%
  • Boiling Heat Transfer 66%
  • Pool Boiling 66%
  • Heating Surface 66%
  • Heat Transfer 66%
  5 被引用数 (Scopus)