堀澤 秀之

Horisawa Hideyuki

  • 教授
  • 学位:博士(工学)

基本情報

所属

  • Undergraduate School of Engineering / Department of Aeronautics and Astronautics Aerospace Course
  • Graduate School of Science and Technology / Course of Science and Technology
  • Graduate School of Engineering / Course of Mechanical Engineering

ジャンル

  • Space Development

研究と関連するSDGs

  • Affordable and Clean Energy
  • Industry, Innovation and Infrastructure

詳細情報

研究キーワード

  • Combustion Engineering
  • Plasma and Laser Processing
  • Propulsion Engineering

研究分野

  • Aerospace, marine, and maritime Engineering Aerospace engineering
  • Nanotechnology/Materials Material fabrication and microstructure control
  • Manufacturing technology (mechanical, electrical/electronic, chemical engineering) Thermal engineering

論文

Ion energy distribution measurement for miniaturized low-power Hall thruster

Hollow anode characterization for low-power miniaturized SPT Hall thruster

Characterization of miniaturized low-power anode layer Hall thrusters

Coaxial Short-pulse Laser-assisted Pulsed Plasma Thruster Characterization

Hollow anode characterization for low-power Hall thrusters

Miniaturization of Low Power Hall Thrusters

UV-LED Microthruster through Interaction of Ultraviolet Photons and Solid Polymers

Impact of Hollow Anode Geometries on Characteristics of Miniature Low-Power Magnetic-Layer Hall Thruster

A Photon-driven Microthruster through Interaction of Ultraviolet Light-emitting Diodes and Solid Polymers

Hollow anode geometries for small-size very low-power Hall thrusters

Acceleration Characteristics of Ions Exhausted from Short Pulse Coaxial Laser-Assisted Pulse Plasma Thruster

Evaluation of Low Power Operating Characteristics of Miniature Anode-Layer Hall Thruster by Experiment and Particle Simulation

Development of Laser Thermal Microthruster with Diode-Laser Coupled Fiber-Tip Heat Source

Study on High-Repetition-Rate Diagnostics of Laser Ablation Plasma

Relationship of current distribution of magnetopause and thrust characteristics in multipole magnetic sail

Indirect Electrothermal Acceleration of a Cold Gas Jet through Interaction of an arcjet Exhaust Flow for Space Propulsion Applications

書籍等出版物

  • Chap. 6 : Study of Very Low Power Arcjets
  • Section 4-2 : Application of Laser Beams for Combustion

共同研究・競争的資金等の研究課題

Development of All-solid State Miniature uvLED Plasma Thrusters using Photo-chamical Processes

Non-linear acceleration mechanism of photo-interaction of ultraviolet diodes and advanced materials

Microfabrication of mega-pixcel micro-plasmajets and their potentials for medical applications

Novel Acceleration Mechanisms and Plasma Propulsion Applications through Interactions of Ultra-short-pulse Discharges and Matters

Study of MPD Thruster System for Future High-power Space Explorations

Investigations of Laser Ablation Thrusters for Accurate Attitude Control of Spacecraft

Throttleable solid propellant microthruster using laser heating

Laser Micro Thruster using Metallic Propellants

Performance Evaluation of Magnetoplasma Sail

Experimental Study of a Laser Micro-Thruster for Precise Attitude Control of Spacecraft

Characterization of Laser-Electric Hybrid Acceleration Plasma Thruster and System Development for Spacecraft Applications

Laboratory Experiment of Magnetoplasma Sail for Rapid Deep Space Explorations

Space Propulsion System using Relativistic Plasma Beams through Intense Laser-Solid Nonlinear Interactions

Laser Controlled Solid Propellant Micro-thruster

Manufacturing of Microparts for medical and Dental Use by Plastic working

Study of physics and practical applications of laser-driven in-tube accelerator

Micmfabrication of Sapphire wafers for Sensor Devices with UV Laser Pulses

Fabrication Process for Ni-Ti Shape-Memory-Alloy Fine Tubes Used in Medical Tests

Numerical and Experimental Studies on Non Equilibrium Flows in MPD Arc Jets.

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