Search Results1-20 of  31

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  • MARU Yusuke ID: 9000006945458

    Articles in CiNii:13

    • Aerodynamic Characteristics of Telescopic Aerospikes with Multiple-Row-Disk (2007)
    • Aerodynamic Characteristics of Conical Nose with Axisymmetric Cavities (2007)
    • Flight Test of Supersonic Air Breathing Engine using High Altitude Balloon (2009)
  • MARU Yusuke ID: 9000017383386

    Articles in CiNii:9

    • Fundamental Study on Coking Characteristics of LNG Rocket Engines (2009)
    • Research and Development of Detonation Engines and Its Present Status (2016)
    • Propulsion Base Technology: Fundamental Study on Coking Characteristics of LNG Rocket Engines. (2009)
  • MARU Yusuke ID: 9000265258283

    Institute of Space and Astronautical Science, JAXA, Sagamihara (2014 from CiNii)

    Articles in CiNii:1

    • Droplet Array Combustion Experiment under Microgravity by Using the Balloon Operated Vehicle (2014)
  • MARU Yusuke ID: 9000283632931

    Institute of Space and Astronautical Science, JAXA (2014 from CiNii)

    Articles in CiNii:1

    • Aerodynamic Characteristics of Simplified Waveriders (2014)
  • MARU Yusuke ID: 9000304305980

    宇宙航空研究開発機構宇宙科学研究所 (2014 from CiNii)

    Articles in CiNii:1

    • 2214 Concept Design Method by Combination of Products and Operations : Report 1: Definition of Framework for Concept Design (2014)
  • MARU Yusuke ID: 9000304305987

    宇宙航空研究開発機構宇宙科学研究所 (2014 from CiNii)

    Articles in CiNii:1

    • 2215 Concept Design Method by Combination of Products and Operations : Report 2: Parameter Sensitivity Analysis Method for Concept Design (2014)
  • MARU Yusuke ID: 9000311505247

    (独)宇宙航空研究開発機構 (2015 from CiNii)

    Articles in CiNii:1

    • Development and Flight Experiment Results of Microgravity Experiment System with One-Directional Drag-Free Control using High Altitude Balloon (2015)
  • MARU Yusuke ID: 9000323299897

    The Institute of Space and Astronautical Science, JAXA (2016 from CiNii)

    Articles in CiNii:1

    • Conceptual Study on Hydrogen-Based Integration of Propulsion and Power in Space Transportation System (2016)
  • MARU Yusuke ID: 9000329012581

    宇宙航空研究開発機構 宇宙科学研究所 (2016 from CiNii)

    Articles in CiNii:1

    • Overview of ISAS/JAXA Wind Tunnel Facility (2016)
  • MARU Yusuke ID: 9000345199441

    Institute of Space and Astronautical Science, JAXA (2016 from CiNii)

    Articles in CiNii:1

    • Development of Supersonic Parachute for Japanese Mars Rover Mission (2016)
  • MARU Yusuke ID: 9000345347396

    国立研究開発法人 宇宙航空研究開発機構 (2017 from CiNii)

    Articles in CiNii:1

    • Development of Supersonic Parachute for Landing Mission on Mars (2017)
  • MARU Yusuke ID: 9000365497100

    Articles in CiNii:1

    • Interference Analysis of Dual-band WiCoPT System for Wireless Sensor Network in RVT (2015)
  • MARU Yusuke ID: 9000383089339

    ISAS / JAXA (2018 from CiNii)

    Articles in CiNii:1

    • Preliminary System Design of Small Lunar Landing Demonstrator SLIM (2018)
  • MARU Yusuke ID: 9000383124772

    Institute of Space and Astronautical Science, JAXA (2018 from CiNii)

    Articles in CiNii:1

    • Anomaly Detection Configured as a Combination of State Observer and Mahalanobis-Taguchi Method for a Rocket Engine (2018)
  • MARU Yusuke ID: 9000386208127

    Japan Aerospace Exploration Agency (2017 from CiNii)

    Articles in CiNii:1

    • Flow measurement system for highly compressed (84 MPa) liquid hydrogen (2017)
  • MARU Yusuke ID: 9000386208236

    Japan Aerospace Exploration Agency (2017 from CiNii)

    Articles in CiNii:1

    • Dispersion Behaviour of Highly Compressed Liquid Hydrogen from a Pinhole (2017)
  • MARU Yusuke ID: 9000386336059

    SOKENDAI (The Graduate University for Advanced Studies)|Japan Aerospace Exploration Agency (JAXA) (2018 from CiNii)

    Articles in CiNii:1

    • A Landing Method with Intentional Tumbling for Small Lunar Lander (2018)
  • MARU Yusuke ID: 9000391520396

    国立研究開発法人 宇宙航空研究開発機構 (2017 from CiNii)

    Articles in CiNii:1

    • Wind Tunnel Testing of Parachutes at Transonic and Supersonic Speed (2017)
  • MARU Yusuke ID: 9000392157914

    Japan Aerospace Exploration Agency, Institute of Space and Astronautical Science (2016 from CiNii)

    Articles in CiNii:1

    • Hydrogen Leak Detection in a Hydrogen-fueled Reusable Rocket (2016)
  • MARU Yusuke ID: 9000392174531

    Japan Aerospace Exploration Agency. Inst. of Space and Astronautical Science (2016 from CiNii)

    Articles in CiNii:1

    • Wind Tunnel Testing of Parachutes at Transonic and Supersonic Speed (2016)
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