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

• 2025

  Multidisciplinary System Design Optimization of Interplanetary Transfer Vehicle from Geostationary Transfer Orbit to Low Mars Orbit

  Yeo, S. H., Takao, Y., Suenaga, K., Ozawa, T., Matsuura, T., Mori, H., Morano, J. A. & Ogawa, H., 2025, AIAA Science and Technology Forum and Exposition, AIAA SciTech Forum 2025. American Institute of Aeronautics and Astronautics Inc, AIAA, (AIAA Science and Technology Forum and Exposition, AIAA SciTech Forum 2025).

  研究成果: 書籍/レポート タイプへの寄稿 › 会議への寄与

• Multidisciplinary System Design Optimization of Interplanetary Vehicles with Solar Electric Propulsion

  Takao, Y., Matsuura, T., Yeo, S. H., Ozawa, T., Suenaga, K., Mori, H., Morano, J. A. & Ogawa, H., 2025, AIAA Science and Technology Forum and Exposition, AIAA SciTech Forum 2025. American Institute of Aeronautics and Astronautics Inc, AIAA, (AIAA Science and Technology Forum and Exposition, AIAA SciTech Forum 2025).

  研究成果: 書籍/レポート タイプへの寄稿 › 会議への寄与

  • Electric Propulsion 100%
  • Design Optimization 100%
  • Solar Electric Propulsion 100%
  • Optimization Method 50%
  • Time-of-Flight 50%
• 2024

  Close Approach Analysis Method Considering Attitude and Shape Using Dual Quaternions

  Kajikawa, T., Yoshimura, Y., Chen, H. & Hanada, T., 2024, AIAA SciTech Forum and Exposition, 2024. American Institute of Aeronautics and Astronautics Inc, AIAA, (AIAA SciTech Forum and Exposition, 2024).

  研究成果: 書籍/レポート タイプへの寄稿 › 会議への寄与

  • Rotational Motion 100%

• Concept Study for Japanese Comet Sample Return Exploration in the 2030s

  Saiki, T., Tsuda, Y., Mori, O., Aiko, Y., Mastumoto, J., Kikuchi, S., Takao, Y., Kurokawa, H., Shimaki, Y., Sakatani, N., Fukai, R. & Okada, T., 2024, IAF Space Exploration Symposium - Held at the 75th International Astronautical Congress, IAC 2024. International Astronautical Federation, IAF, p. 731-737 7 p. (Proceedings of the International Astronautical Congress, IAC; vol. 1A).

  研究成果: 書籍/レポート タイプへの寄稿 › 会議への寄与

  • Sample Return Mission 100%
  • Spacecraft Instrument 100%
  1 被引用数 (Scopus)

• Multidisciplinary System Design Optimization for Lunar Transportation Missions via Surrogate-Assisted Evolutionary Algorithms

  Takao, Y., Ozawa, T., Yeo, S. H., Suenaga, K., Bandera, A. Y. & Ogawa, H., 2024, AIAA SciTech Forum and Exposition, 2024. American Institute of Aeronautics and Astronautics Inc, AIAA, (AIAA SciTech Forum and Exposition, 2024).

  研究成果: 書籍/レポート タイプへの寄稿 › 会議への寄与

  • Multidisciplinary Design Optimization 100%
  • Payload Mass 49%
  • Space Solution 49%
  3 被引用数 (Scopus)

• Physical Insights into Downsized Nozzle Geometry for Microwave Electrothermal Thruster via Evolutionary Algorithms

  Suenaga, K., Yeo, S. H., Ozawa, T. & Ogawa, H., 2024, AIAA SciTech Forum and Exposition, 2024. American Institute of Aeronautics and Astronautics Inc, AIAA, (AIAA SciTech Forum and Exposition, 2024).

  研究成果: 書籍/レポート タイプへの寄稿 › 会議への寄与

  • Nozzle Design 100%
  • High Thrust 100%
  • Flow Velocity 100%
  • Optimal Geometry 100%
• 2023

  Characterization of Shock-Induced Mixing Enhancement for Transverse Injection in Scramjet Engines

  Fujio, C. & Ogawa, H., 2023, 25th AIAA International Space Planes and Hypersonic Systems and Technologies Conference, 2023. American Institute of Aeronautics and Astronautics Inc, AIAA, (25th AIAA International Space Planes and Hypersonic Systems and Technologies Conference, 2023).

  研究成果: 書籍/レポート タイプへの寄稿 › 会議への寄与

  • Oblique Shock 100%
  • Mixing Region 50%
  1 被引用数 (Scopus)

• Multi-objective Design Optimization and Uncertainty Analysis of a Downscaled Cusped Field Thruster

  Hyun Yeo, S. & Ogawa, H., 2023, The Proceedings of the 2021 Asia-Pacific International Symposium on Aerospace Technology APISAT 2021, Volume 2. Lee, S., Han, C., Choi, J.-Y., Kim, S. & Kim, J. H. (eds.). Springer Science and Business Media Deutschland GmbH, p. 1397-1410 14 p. (Lecture Notes in Electrical Engineering; vol. 913).

  研究成果: 書籍/レポート タイプへの寄稿 › 会議への寄与

  • Thruster 100%
  • Fields 80%
  • Design Optimization 60%
  • Simulation 40%
  • Performance 40%

• Physical Insight into Microwave Electrothermal Thruster Startup via Multi-Objective Design Optimization and Plasma Simulation

  Ozawa, T., Yeo, S. H. & Ogawa, H., 2023, AIAA SciTech Forum and Exposition, 2023. American Institute of Aeronautics and Astronautics Inc, AIAA, (AIAA SciTech Forum and Exposition, 2023).

  研究成果: 書籍/レポート タイプへの寄稿 › 会議への寄与

  • Plasma Simulation 100%
  • Electric Field 100%
  • Blood Plasma 100%
  • Design Optimization 100%
  • Resonator 100%
  2 被引用数 (Scopus)
• 2022

  Design and Numerical Investigation of a Hypersonic Waverider based Entry, Descent, and Landing Architecture Assisted by Supersonic Retro-Propulsion

  Ghosh, D. & Ogawa, H., 2022, 26th AIAA Aerodynamic Decelerator Systems Technology Conference and Seminar, ADSTCS 2022. American Institute of Aeronautics and Astronautics Inc, AIAA, AIAA 2022-2734. (26th AIAA Aerodynamic Decelerator Systems Technology Conference and Seminar, ADSTCS 2022).

  研究成果: 書籍/レポート タイプへの寄稿 › 会議への寄与

  • Supersonics 100%
  • Landing 100%
  • Hypersonics 66%
  • Design 66%
  • Architecture 66%

• Scramjet Intake Design Based on Exit Flow Profile via Global Optimization and Deep Learning toward Inverse Design

  Fujio, C. & Ogawa, H., 2022, AIAA SciTech Forum 2022. American Institute of Aeronautics and Astronautics Inc, AIAA, AIAA 2022-1408. (AIAA Science and Technology Forum and Exposition, AIAA SciTech Forum 2022).

  研究成果: 書籍/レポート タイプへの寄稿 › 会議への寄与

  • Supersonic Combustion Ramjet Engines 100%
  • Mixing 100%
  • Design 100%
  • Combustion 66%
  • Fuel 66%
  7 被引用数 (Scopus)
• 2021

  Application of Halo Orbit on Extension for Launch Window Limited by Direct Earth-Mars Transfer

  Xu, Z., Bando, M., Ogawa, H. & Hokamoto, S., 2月 2021, 31st AAS/AIAA Space Flight Mechanics Meeting. AAS 21-300

  研究成果: 書籍/レポート タイプへの寄稿 › 会議への寄与

• Global Optimization of Manifold-Based Transfers to Halo and Butterfly Orbits Using Highly-Parallel GPU Architecture

  Foo, Y., Ogawa, H., Ueda, S. & Bando, M., 8月 2021, 2021 AAS/AIAA Astrodynamics Specialist Conference. AAS 21-675

  研究成果: 書籍/レポート タイプへの寄稿 › 会議への寄与

• Global Trajectory Optimization of Earth-NRHO Transfer Using Weak Stability Boundary via GPU-Based Super-Parallelization

  Ueda, S. & Ogawa, H., 2月 2021, 31st AAS/AIAA Space Flight Mechanics Meeting. AAS 21-320

  研究成果: 書籍/レポート タイプへの寄稿 › 会議への寄与

• Global Trajectory Optimization of Earth-NRHO Transfer via Multiple Impulsive Maneuvers Using Highly Parallel GPU Architecture

  Ueda, S. & Ogawa, H., 8月 2021, 2021 AAS/AIAA Astrodynamics Specialist Conference. AAS 21-668)

  研究成果: 書籍/レポート タイプへの寄稿 › 会議への寄与

• Multidisciplinary System Design;Optimization of Lunar;Surface Access from Cislunar Orbit via Surrogate-Assisted Evolutionary Algorithms Using Highly-Parallel GPU Architecture

  Furutachi, K., Ogawa, H. & Ueda, S., 2月 2021, 31st AAS/AIAA Space Flight Mechanics Meeting. AAS 21-291

  研究成果: 書籍/レポート タイプへの寄稿 › 会議への寄与

• Multi-objective design optimization and analysis of streamline-traced intakes for scramjet-powered ascent flight

  Fujio, C. & Ogawa, H., 2021, AIAA Scitech 2021 Forum. American Institute of Aeronautics and Astronautics Inc, AIAA, p. 1-24 24 p. (AIAA Scitech 2021 Forum).

  研究成果: 書籍/レポート タイプへの寄稿 › 会議への寄与

  • Streamlines 100%
  • Supersonic Combustion Ramjet Engines 75%
  • Design Optimization 50%
  • Design 50%
  • Performance 25%

• MULTIPLE IMPULSE CISLUNAR TRANSFER VIA MULTI-FIDELITY APPROACH USING GPU-BASED SUPER PARALLELIZATION

  Ueda, S. & Ogawa, H., 2021, ASTRODYNAMICS 2020. Wilson, R. S., Shan, J., Howell, K. C. & Hoots, F. R. (eds.). Univelt Inc., p. 5107-5126 20 p. (Advances in the Astronautical Sciences; vol. 175).

  研究成果: 書籍/レポート タイプへの寄稿 › 会議への寄与

  • Transferring 100%
  • Graphics Processing Unit 66%
  • Orbits 33%
  • Determines 33%
  • Optimization 33%

• Multi-point design optimization of busemann based intakes for scramjet-powered ascent flight via surrogate-assisted evolutionary algorithms

  Brahmachary, S. & Ogawa, H., 2021, AIAA Scitech 2021 Forum. American Institute of Aeronautics and Astronautics Inc, AIAA, p. 1-33 33 p. (AIAA Scitech 2021 Forum).

  研究成果: 書籍/レポート タイプへの寄稿 › 会議への寄与

  • Compression Efficiency 100%
  • Algorithm 66%
  • Optimization 66%
  • Design Condition 66%
  • Static Pressure 66%
  2 被引用数 (Scopus)

• Pulse width modulation method applied to nonlinear model predictive control on an under-actuated small satellite

  Kondo, K., Yoshimura, Y., Nagasaki, S., Fukuo, F. S. & Hanada, T., 2021, AIAA Scitech 2021 Forum. American Institute of Aeronautics and Astronautics Inc, AIAA, p. 1-19 19 p. (AIAA Scitech 2021 Forum).

  研究成果: 書籍/レポート タイプへの寄稿 › 会議への寄与

  • Predictive Control Model 100%
  • Small Satellite 75%
  • Pulse Width Modulation 50%
  • Nonlinear Model 50%
  • Actuators 37%
  1 被引用数 (Scopus)

• Survey of Low-Energy Transfers to Lunar Libration Point Orbits with Targeted L1 Transits

  Yang, F., Ogawa, H. & Ueda, S., 8月 2021, 2021 AAS/AIAA Astrodynamics Specialist Conference. AAS 21-675

  研究成果: 書籍/レポート タイプへの寄稿 › 会議への寄与

• 深層学習を用いたスクラムジェットインテーク内部流れ場の予測に関する研究

  寄稿の翻訳タイトル: 深層学習を用いたスクラムジェットインテーク 内部流れ場の予測に関する研究Fujio, C. & Ogawa, H., 7月 2021, 第53回流体力学講演会／第39回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. 3A03

  研究成果: 書籍/レポート タイプへの寄稿 › 会議への寄与
• 2020

  Centreline Reflection of Axisymmetric Shock Waves in Supersonic Ring Wedge Intakes

  Ogawa, H., Fujio, C., Shoesmith, B., Mölder, S., Timofeev, E., Shoev, G. & Ohtani, K., 10月 2020, 20th International Symposium on Advanced Fluid Information (AFI 2020).

  研究成果: 書籍/レポート タイプへの寄稿 › 会議への寄与

• Design optimisation and off-design performance study of an axisymmetric scramjet intake for ascent flight

  Brahmachary, S., Fujio, C., Aksay, M. & Ogawa, H., 12月 2020, 8th International and 47th National Conference on Fluid Mechanics and Fluid Power (FMFP 2020).

  研究成果: 書籍/レポート タイプへの寄稿 › 会議への寄与

• Global Trajectory Optimization Framework via Multi-Fidelity Approach Supported by Machine Learning and Primer Vector Theory for Advanced Space Mission Design

  Ueda, S. & Ogawa, H., 3月 2020, Proceedings of 2020 SICE International Symposium on Control Systems, SICE ISCS 2020. Institute of Electrical and Electronics Engineers Inc., p. 69-76 8 p. 9083488. (Proceedings of 2020 SICE International Symposium on Control Systems, SICE ISCS 2020).

  研究成果: 書籍/レポート タイプへの寄稿 › 会議への寄与

  • Trajectories 100%
  • Space Missions 75%
  • Graphics Processing Unit 50%
  • Central Processing Unit 50%
  • Primer Vector 50%
  2 被引用数 (Scopus)

• Influence of turbulence modeling on combustor flowfield in scramjet mode of RBCC engine

  Salloum, J., Candon, M., Ogawa, H. & Kodera, M., 2020, 23rd AIAA International Space Planes and Hypersonic Systems and Technologies Conference, 2020. American Institute of Aeronautics and Astronautics Inc, AIAA, (23rd AIAA International Space Planes and Hypersonic Systems and Technologies Conference, 2020).

  研究成果: 書籍/レポート タイプへの寄稿 › 会議への寄与

  • Combustor 100%
  • Turbulence 75%
  • Combined-Cycle Engine 75%
  • Performance 50%
  • Injector 50%

• Model predictive approach for detumbling an underactuated satellite

  Kondo, K., Yoshimura, Y., Bando, M., Nagasaki, S. & Hanada, T., 2020, AIAA Scitech 2020 Forum. American Institute of Aeronautics and Astronautics Inc, AIAA, (AIAA Scitech 2020 Forum; vol. 1 PartF).

  研究成果: 書籍/レポート タイプへの寄稿 › 会議への寄与

  Open Access

  • Satellites 100%
  • Control Law 66%
  • Underactuated System 66%
  • Predictive Control Model 66%
  • Computer Simulation 33%
  1 被引用数 (Scopus)

• Multiple Impulse Cislunar Transfer via Multi-Fidelity Approach using GPU-based Super Parallelization

  Satoshi, U. & Ogawa, H., 8月 2020, 2020 Astrodynamics Specialist Conference.

  研究成果: 書籍/レポート タイプへの寄稿 › 会議への寄与

• Multi-target rendezvous optimization for active debris removal via multi-fidelity approach

  Brahmachary, S., Atsuki, T., Ogawa, H., Bang, J., Ahn, J. & Ueda, S., 3月 2020, SICE International Symposium on Control Systems 2020.

  研究成果: 書籍/レポート タイプへの寄稿 › 会議への寄与

• Numerical investigation of upstream cavity enhanced combustion in a scramjet combustor

  Roos, T., Pudsey, A. S., Bricalli, M. G. & Ogawa, H., 2020, 23rd AIAA International Space Planes and Hypersonic Systems and Technologies Conference, 2020. American Institute of Aeronautics and Astronautics Inc, AIAA, (23rd AIAA International Space Planes and Hypersonic Systems and Technologies Conference, 2020).

  研究成果: 書籍/レポート タイプへの寄稿 › 会議への寄与

  • Cavity 100%
  • Performance 29%
  • Fuel 29%
  • Temperature 23%
  • Combustion 23%
  2 被引用数 (Scopus)

• RBCCエンジンにおけるスクラムジェットモード燃焼に関する数値的研究

  寄稿の翻訳タイトル: RBCCエンジンにおけるスクラムジェットモード燃焼に関する数値的研究Katsura, H., Ogawa, H. & Kodera, M., 11月 2020, 日本航空宇宙学会西部支部講演会（2020）論文集. JSASS-2020-S010

  研究成果: 書籍/レポート タイプへの寄稿 › 会議への寄与

• Reduced Order Chemical Kinetic Modeling for a Hydrogen FueledRadical Farming Scramjet

  Mazumdar, R., Ogawa, H. & Pudsey, A., 10月 2020, 5th World Congress on Momentum, Heat and Mass Transfer.

  研究成果: 書籍/レポート タイプへの寄稿 › 会議への寄与
• 2019

  CFD-Coupled 6-DOF Attitude & Trajectory Analysis for Hypersonic Air Vehicles

  Escalante, J., Xu, R., Ogawa, H. & Pudsey, A., 2月 2019, 18th Australian International Aerospace Congress (AIAC18). Melbourne, Australia, p. 64-71

  研究成果: 書籍/レポート タイプへの寄稿 › 会議への寄与

• Investigation of Centreline Shock Reflection in Ring-Shaped Supersonic Intake Geometries

  Ogawa, H., Fujio, C., Brahmachary, S., Watanabe, T. & Watanabe, K., 11月 2019, 19th International Symposium on Advanced Fluid Information (AFI 2019). Sendai, Japan

  研究成果: 書籍/レポート タイプへの寄稿 › 会議への寄与

• Multi-Fidelity Optimisation of Multi-Target Rendezvous Problems by Using GPU Super-Parallelisation

  Brahmachary, S., Atsuki, T., Ogawa, H., Bang, J., Ahn, J. & Ueda, S., 12月 2019, 11th Kyushu-University-KAIST Symposium on Aerospace Engineering.

  研究成果: 書籍/レポート タイプへの寄稿 › 会議への寄与

• Multi-Objective Optimisation of NRHO-LLO Orbit Transfer via Surrogate-Assisted Evolutionary Algorithms

  Rozek, M., Ogawa, H., Ueda, S. & Ikenaga, T., 2月 2019, 27th International Symposium on Space Flight Dynamics (ISSFD). Melbourne, Australia, p. 1001-1007

  研究成果: 書籍/レポート タイプへの寄稿 › 会議への寄与

• Numerical Analysis of Thermal Loading in Dual-Bell Rocket Nozzles

  Hewitt, C., Ogawa, H. & Bricalli, M., 2月 2019, 18th Australian International Aerospace Congress (AIAC18). Melbourne, Australia, p. 34-39

  研究成果: 書籍/レポート タイプへの寄稿 › 会議への寄与

• Numerical and Experimental Investigation of Centreline Shock Reflection in Ring-Shaped Supersonic Intake Geometries

  Ogawa, H., Fujio, C., Brahmachary, S., Watanabe, T. & Ohtani, K., 11月 2019, 19th International Symposium on Advanced Fluid Information (AFI 2019).

  研究成果: 書籍/レポート タイプへの寄稿 › 会議への寄与

• Numerical Investigation on Axisymmetric and Planar Shock Reflections in Steady Viscous Flow

  Shoev, G. & Ogawa, H., 7月 2019, 32nd International Symposium on Shock Waves. Singapore, OR-15-334

  研究成果: 書籍/レポート タイプへの寄稿 › 会議への寄与

• Performance Design Optimization of RBCC Combustor in Ramjet and Scramjet Operation via Surrogate-Based Evolutionary Algorithms

  Candon, M., Driscoll, P., Salloum, J., Ogawa, H. & Kodera, M., 9月 2019, 24th ISABE Conference (ISABE 2019). Canberra, Australia, ISABE-2019-24369

  研究成果: 書籍/レポート タイプへの寄稿 › 会議への寄与
• 2018

  Analysis of Effects of Magnet Configurations for Downscaled Cusped Field Thruster via Surrogate Assisted Evolutionary Algorithms

  Yeo, S. H. & Ogawa, H., 9月 2018, 18th Australian Space Research Conference. Gold Coast, Australia

  研究成果: 書籍/レポート タイプへの寄稿 › 会議への寄与

• An experimental study on gust load alleviation using passive ventilation wing concept

  Tani, Y., Seki, S. & Aso, S., 2018, AIAA Aerospace Sciences Meeting. 210059 ed. American Institute of Aeronautics and Astronautics Inc, AIAA, (AIAA Aerospace Sciences Meeting, 2018; vol. 0, no. 210059).

  研究成果: 書籍/レポート タイプへの寄稿 › 会議への寄与

  • Gust Load 100%
  • Wings 80%
  • Mechanisms 40%
  • Aerodynamic Force 40%
  • Models 20%
  7 被引用数 (Scopus)

• A study on high performance hybrid rocket engine with multi-section swirl injection method for space propulsion system

  Aso, S., Tani, Y., Saiga, T. S., Arakawa, R. & Shimada, T., 2018, AIAA Aerospace Sciences Meeting. 210059 ed. American Institute of Aeronautics and Astronautics Inc, AIAA, (AIAA Aerospace Sciences Meeting, 2018; vol. 0, no. 210059).

  研究成果: 書籍/レポート タイプへの寄稿 › 会議への寄与

  • Hybrid Rocket Engine 100%
  • Injection 100%
  • Regression 40%
  • Fuel 40%
  • Swirling Flow 40%
  2 被引用数 (Scopus)

• Characteristics of Centreline Shock Reflection in Stunted Busemann Intakes

  Ogawa, H., Shoesmith, B., Mölder, S., Timofeev, E., Shoev, G. & Ohtani, K., 11月 2018, 18th International Symposium on Advanced Fluid Information (AFI 2018). Sendai, Japan

  研究成果: 書籍/レポート タイプへの寄稿 › 会議への寄与

• Feasibility study on shared design of hypersonic transport and booster of TSTO for reduction of development cost

  Aso, S., Tani, Y. & Hirayama, T., 2018, AIAA Aerospace Sciences Meeting. 210059 ed. American Institute of Aeronautics and Astronautics Inc, AIAA, (AIAA Aerospace Sciences Meeting, 2018; vol. 0, no. 210059).

  研究成果: 書籍/レポート タイプへの寄稿 › 会議への寄与

  • Hypersonics 100%
  • Development 75%
  • Design 75%
  • Development Cost 75%
  • Space Transportation 75%
  1 被引用数 (Scopus)

• Passive ventilation flow control for aircraft gust load alleviation

  Tani, Y., Seki, S. & Aso, S., 2018, 31st Congress of the International Council of the Aeronautical Sciences, ICAS 2018. International Council of the Aeronautical Sciences, (31st Congress of the International Council of the Aeronautical Sciences, ICAS 2018).

  研究成果: 書籍/レポート タイプへの寄稿 › 会議への寄与

  • Gust Load 100%
  • Wings 60%
  • Mechanisms 40%
  • Aerodynamic Force 40%
  • Models 20%
• 2017

  A Systems Engineering Approach to Spacecraft Trajectory Optimisation

  Coulloupas, G. & Ogawa, H., 4月 2017, CubeSat 2017.

  研究成果: 書籍/レポート タイプへの寄稿 › 会議への寄与

• Environmental estimation on sub-millimeter-size debris using in-situ measurement data

  Furumoto, M., Nakano, S., Fujita, K. & Hanada, T., 2017, Spaceflight Mechanics 2017. Sims, J. A., Leve, F. A., McMahon, J. W. & Guo, Y. (eds.). Univelt Inc., p. 3441-3450 10 p. (Advances in the Astronautical Sciences; vol. 160).

  研究成果: 書籍/レポート タイプへの寄稿 › 会議への寄与

  • Debris 100%
  • Size 57%
  • Model 42%
  • Models 42%
  • Estimation 42%

• Estimation of orbital parameters of broken-up objects from In-situ debris measurement

  Kodama, Y., Furumoto, M., Fujita, K. & Hanada, T., 2017, 68th International Astronautical Congress, IAC 2017: Unlocking Imagination, Fostering Innovation and Strengthening Security. International Astronautical Federation, IAF, p. 3982-3996 15 p. (Proceedings of the International Astronautical Congress, IAC; vol. 6).

  研究成果: 書籍/レポート タイプへの寄稿 › 会議への寄与

  • Debris 100%
  • Orbital Parameter 80%
  • Estimates 80%
  • Measurement 60%
  • Satellites 60%
  1 被引用数 (Scopus)

• Flight trajectory analysis on advanced morphing space transportation system for wider cross range and down range with trimmed flight

  Aso, S., Tani, Y. & Shiomi, K., 2017, 68th International Astronautical Congress, IAC 2017: Unlocking Imagination, Fostering Innovation and Strengthening Security. International Astronautical Federation, IAF, p. 1489-1495 7 p. (Proceedings of the International Astronautical Congress, IAC; vol. 3).

  研究成果: 書籍/レポート タイプへの寄稿 › 会議への寄与

  • Flight Trajectory 100%
  • Cross-Range 100%
  • Aerodynamic Performance 66%
  • Landing 66%
  • Lift to Drag Ratio 66%