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

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

Study on the soot suppression in a hydrocarbon turbulent diffusion flame by corona discharges

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

A Chemically Augmented Arcjet Thruster with Exotic Propellants

Evaluation of Coaxial Short-pulse Laser-assisted Pulsed Plasma Thruster

Laser Ablation Plasma Diagnostics for Electrostatic Acceleration

Interaction of Ultraviolet Light-emitting Diodes and Solid Polymers for Micropropulsion Applications 掲載誌名

Preliminary results of magnetic field measurements on multi-coil magnetic sail in laboratory experiment

Acceleration Characteristics of a Supersonic Free Jet through a Plasmajet

Characteristics of a Coaxial Short-pulse Laser-assisted Pulsed Plasma Thruster

Acceleration Characteristic of Laser Ablation Plasma by Alternating Electrostatic Field

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

Fundamental Study on Plasma Thrusters

Fundamental Study on Laser Machining

Fundamental Study on Laser Propulsion

Fundamental Study on Laser Propulsion

Study on LASER Machining

Study on Development and Evaluation of very Low-Power Arcjets

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Inquiries about coverage or research

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