Takahiro Shinya
Current Organizations / Institutes
The organizations/institutes from the scholar's latest article
Previous Organizations / Institutes
The organizations / institutes from the scholar's other articles in the past ten years
Research Subjects
Takahiro Shinya has a total of 189 co-authors. Here are the top co-authors by number of shared publications:
Ken Kajiwara
7 shared publications- Yuichi Takase
Tokamak Energy Ltd
6 shared publications - Akira Ejiri
The University of Tokyo, Kashiwa 277-8561, Japan
5 shared publications H. Kakuda
The University of Tokyo, Kashiwa 277-8561, Japan
5 shared publicationsK. Imamura
The University of Tokyo, Kashiwa 277-8561, Japan
5 shared publications- Ryosuke Ikeda
National Institute for Quantum Science and Technology, 801-1 Mukoyama, Naka 311-0193, Japan
5 shared publications
Latest Publications
- Open Access
- 16 October 2026
- Published by Elsevier in SSRN Electronic Journal
Millimeter Wave Absorption Measurement of TiO2 Coating for Low Reflection Dummy Load
Accurate reflectivity data of millimeter wave absorber materials are essential for predicting heat-flux distributions and optimizing the design of dummy loads (DLs) used in electron cyclotron resonance heating (ECRH) systems. However, conventional millimeter wave reflectivity measurements typically exhibit uncertainties of approximately ±5%, which are insufficient for reliable design. In this study, a high-accuracy reflectivity measurement was developed and applied to thermally sprayed TiO2 coatings. Measurements were performed at 110 GHz, corresponding to the operating frequency of the JT-60SA ECRH system. To improve measurement accuracy, an HE11-mode launcher was employed to suppress beam divergence during free-space propagation, and a two-dimensional scanning measurement was performed to capture the full reflected-wave intensity distribution. In addition, a reference-based calibration method using a copper reflector eliminated the need for direct estimation of the incident wave intensity and reduced the influence of source-power fluctuations. Reflectivities were measured for incident angles between 30° and 65° under both S- and P-polarized conditions, achieving an uncertainty of less than ±0.8%. The measured data were successfully approximated using a Fresnel-based model with a single fitting parameter. The resulting reflectivities were implemented in ray-tracing and thermal analyses and validated through comparisons with infrared-camera and calorimetric measurements obtained during 500 kW high-power experiments. Good agreement was obtained for temperature-rise distributions, temporal temperature evolution, and absorbed-power fractions. These results demonstrate that the proposed method provides reliable reflectivity data for predicting heat-flux distributions and power-absorption characteristics and serves as a powerful tool for the design and optimization of low-reflection DLs.
- 16 October 2026
- Published by Elsevier in SSRN Electronic Journal
Open AccessMillimeter Wave Absorption Measurement of TiO2 Coating for Low Reflection Dummy Load
Accurate reflectivity data of millimeter wave absorber materials are essential for predicting heat-flux distributions and optimizing the design of dummy loads (DLs) used in electron cyclotron resonance heating (ECRH) systems. However, conventional millimeter wave reflectivity measurements typically exhibit uncertainties of approximately ±5%, which are insufficient for reliable design. In this study, a high-accuracy reflectivity measurement was developed and applied to thermally sprayed TiO2 coatings. Measurements were performed at 110 GHz, corresponding to the operating frequency of the JT-60SA ECRH system. To improve measurement accuracy, an HE11-mode launcher was employed to suppress beam divergence during free-space propagation, and a two-dimensional scanning measurement was performed to capture the full reflected-wave intensity distribution. In addition, a reference-based calibration method using a copper reflector eliminated the need for direct estimation of the incident wave intensity and reduced the influence of source-power fluctuations. Reflectivities were measured for incident angles between 30° and 65° under both S- and P-polarized conditions, achieving an uncertainty of less than ±0.8%. The measured data were successfully approximated using a Fresnel-based model with a single fitting parameter. The resulting reflectivities were implemented in ray-tracing and thermal analyses and validated through comparisons with infrared-camera and calorimetric measurements obtained during 500 kW high-power experiments. Good agreement was obtained for temperature-rise distributions, temporal temperature evolution, and absorbed-power fractions. These results demonstrate that the proposed method provides reliable reflectivity data for predicting heat-flux distributions and power-absorption characteristics and serves as a powerful tool for the design and optimization of low-reflection DLs.
- Open Access
- 17 March 2026
- Published by IOP Publishing in Nuclear Fusion
- Vol. 66 (4) , 046017
Demonstration of high-power gyrotron operation at 203 and 236 GHz toward future fusion devices
Gyrotrons having a high output-frequency of more than 200 GHz will be necessary for future fusion devices, such as the DEMO reactor. At 170 GHz, gyrotrons for ITER achieved a high power of 1 MW with a high electrical efficiency of approximately 50% (oscillation efficiency of approximately 30%) in a long pulse operation. At frequencies higher than 200 GHz, no gyrotrons have achieved ITER-like performance, which this study attempted to demonstrate using a prototype multi-frequency gyrotron for 170 GHz, 203 GHz, and 236 GHz. At 203 GHz, an output power of 0.87 MW was achieved at the gyrotron window with an oscillation efficiency of 25% and an electrical efficiency of 41% in a long pulse operation of 100 s. Although this performance is lower than that of the ITER gyrotrons at 170 GHz, this study represents the first demonstration that ITER-like performance is achievable at frequencies above 200 GHz. In addition, short 1 ms pulse tests at 236 GHz achieved an output power of 1 MW.
- 17 March 2026
- Published by IOP Publishing in Nuclear Fusion
- Vol. 66 (4) , 046017
Open AccessDemonstration of high-power gyrotron operation at 203 and 236 GHz toward future fusion devices
Gyrotrons having a high output-frequency of more than 200 GHz will be necessary for future fusion devices, such as the DEMO reactor. At 170 GHz, gyrotrons for ITER achieved a high power of 1 MW with a high electrical efficiency of approximately 50% (oscillation efficiency of approximately 30%) in a long pulse operation. At frequencies higher than 200 GHz, no gyrotrons have achieved ITER-like performance, which this study attempted to demonstrate using a prototype multi-frequency gyrotron for 170 GHz, 203 GHz, and 236 GHz. At 203 GHz, an output power of 0.87 MW was achieved at the gyrotron window with an oscillation efficiency of 25% and an electrical efficiency of 41% in a long pulse operation of 100 s. Although this performance is lower than that of the ITER gyrotrons at 170 GHz, this study represents the first demonstration that ITER-like performance is achievable at frequencies above 200 GHz. In addition, short 1 ms pulse tests at 236 GHz achieved an output power of 1 MW.
- 20 December 2025
- Published by Elsevier in Aerospace Science and Technology
- Vol. 170
Observation of abnormal discharge formation in microwave rocket and its quantitative impact on thrust performance
- 20 December 2025
- Published by Elsevier in Aerospace Science and Technology
- Vol. 170
Observation of abnormal discharge formation in microwave rocket and its quantitative impact on thrust performance
- Open Access
Launch Experiment of Microwave Rocket Equipped with Six-Staged Reed Valve Air-Breathing System
Millimeter-wave-supported detonation (MSD) is a unique detonation phenomenon driven by a supersonically propagating ionization front, sustained by intense millimeter-wave beams. Microwave Rocket, which utilizes MSD to generate thrust from atmospheric air in a pulse detonation engine (PDE) cycle, is a promising low-cost alternative to conventional chemical propulsion systems for space transportation. However, insufficient air intake during repetitive PDE cycles has limited achievable thrust performance. To address this issue, a model equipped with a six-stage reed valve system (36 valves in total) was developed to ensure sufficient air intake, which measured 500 mm in length, 28 mm in radius, and 539 g in weight. Launch demonstration experiments were conducted using a 170 GHz, 550 kW gyrotron developed at the National Institutes for Quantum Science and Technology (QST). Continuous thrust was successfully generated by irradiating up to 50 pulses per experiment at each frequency between 75 and 150 Hz, in 25 Hz increments, corresponding duty cycles ranging from 0.09 to 0.18. A maximum thrust of 9.56 N and a momentum coupling coefficient of 116 N/MW were obtained. These values represent a fourfold increase compared to previous launch experiments without reed valves, thereby demonstrating the effectiveness of the reed valve configuration in enhancing thrust performance.Open AccessLaunch Experiment of Microwave Rocket Equipped with Six-Staged Reed Valve Air-Breathing System
Millimeter-wave-supported detonation (MSD) is a unique detonation phenomenon driven by a supersonically propagating ionization front, sustained by intense millimeter-wave beams. Microwave Rocket, which utilizes MSD to generate thrust from atmospheric air in a pulse detonation engine (PDE) cycle, is a promising low-cost alternative to conventional chemical propulsion systems for space transportation. However, insufficient air intake during repetitive PDE cycles has limited achievable thrust performance. To address this issue, a model equipped with a six-stage reed valve system (36 valves in total) was developed to ensure sufficient air intake, which measured 500 mm in length, 28 mm in radius, and 539 g in weight. Launch demonstration experiments were conducted using a 170 GHz, 550 kW gyrotron developed at the National Institutes for Quantum Science and Technology (QST). Continuous thrust was successfully generated by irradiating up to 50 pulses per experiment at each frequency between 75 and 150 Hz, in 25 Hz increments, corresponding duty cycles ranging from 0.09 to 0.18. A maximum thrust of 9.56 N and a momentum coupling coefficient of 116 N/MW were obtained. These values represent a fourfold increase compared to previous launch experiments without reed valves, thereby demonstrating the effectiveness of the reed valve configuration in enhancing thrust performance. - 9 May 2025
- Published by Elsevier in Fusion Engineering and Design
- Vol. 217
Identifying parasitic oscillations at 570 and 600 MHz in a 170-GHz gyrotron collector
- 9 May 2025
- Published by Elsevier in Fusion Engineering and Design
- Vol. 217
Identifying parasitic oscillations at 570 and 600 MHz in a 170-GHz gyrotron collector
- Open Access
- 7 May 2025
- Published by Elsevier in Acta Astronautica
- Vol. 234, 410-418
Experimental evaluation of a reed valve air intake system for microwave rocket in ground-static tests
- 7 May 2025
- Published by Elsevier in Acta Astronautica
- Vol. 234, 410-418
Open AccessExperimental evaluation of a reed valve air intake system for microwave rocket in ground-static tests
- Open Access
- 9 May 2023
- Published by IOP Publishing in Nuclear Fusion
- Vol. 63 (6) , 066028
Multi-frequency, megawatt-power gyrotron to facilitate a wide range of operations at ITER
High-power (1 MW), long-pulse operations up to 300 s were demonstrated by multi-frequency oscillations at 170 GHz, 137 GHz, and 104 GHz. A multi-frequency gyrotron based on the design of the ITER gyrotron has been developed and studied. By redesigning the built-in mode convertor and internal mirrors of the ITER gyrotron, the internal scattered power of the gyrotron was reduced while maintaining the same output beam size and beam direction for the three frequencies. In addition, the mirrors of a matching optics unit were designed to efficiently couple the RF beam at 170 GHz, 137 GHz, and 104 GHz oscillations to a waveguide 50 mm in diameter, the same size that will be used in ITER. An HE 11 mode content of ∼94% was achieved for the three frequencies. Output powers of 1 MW at 170 GHz and 137 GHz, and 0.9 MW at 104 GHz were demonstrated up to 300 s. These oscillation frequencies can facilitate in a wide range of toroidal magnetic field operations at ITER, including plasma start-up and electron heating and current drive.
- 9 May 2023
- Published by IOP Publishing in Nuclear Fusion
- Vol. 63 (6) , 066028
Open AccessMulti-frequency, megawatt-power gyrotron to facilitate a wide range of operations at ITER
High-power (1 MW), long-pulse operations up to 300 s were demonstrated by multi-frequency oscillations at 170 GHz, 137 GHz, and 104 GHz. A multi-frequency gyrotron based on the design of the ITER gyrotron has been developed and studied. By redesigning the built-in mode convertor and internal mirrors of the ITER gyrotron, the internal scattered power of the gyrotron was reduced while maintaining the same output beam size and beam direction for the three frequencies. In addition, the mirrors of a matching optics unit were designed to efficiently couple the RF beam at 170 GHz, 137 GHz, and 104 GHz oscillations to a waveguide 50 mm in diameter, the same size that will be used in ITER. An HE 11 mode content of ∼94% was achieved for the three frequencies. Output powers of 1 MW at 170 GHz and 137 GHz, and 0.9 MW at 104 GHz were demonstrated up to 300 s. These oscillation frequencies can facilitate in a wide range of toroidal magnetic field operations at ITER, including plasma start-up and electron heating and current drive.
- 24 September 2021
- Published by IOP Publishing in Nuclear Fusion
- Vol. 61 (10) , 106031
Progress on performance tests of ITER gyrotrons and design of dual-frequency gyrotrons for ITER staged operation plan
- 24 September 2021
- Published by IOP Publishing in Nuclear Fusion
- Vol. 61 (10) , 106031
Progress on performance tests of ITER gyrotrons and design of dual-frequency gyrotrons for ITER staged operation plan
- 17 August 2021
- Published by Institute of Electrical and Electronics Engineers (IEEE) in IEEE Transactions on Plasma Science
- Vol. 49 (9) , 2987-2996
Functional Overview of the RF Power System for the LIPAc RFQ
Design, development, manufacturing, and test activities of the RF power system (RFPS) for Linear IFMIF Prototype Accelerator (LIPAc) were completed in Europe. Installation and commissioning activities were carried out at the International Fusion Materials Irradiation Facility-Engineering Validation and Engineering Design Activities (IFMIF/EVEDA) site in Rokkasho, Japan. Challenging IFMIF requirements led to a number of innovations during design and development. Commissioning required a major effort on calibration and fine setting and led to development of new functionalities. The RFPS was validated under full power and 125-mA deuteron beam loading conditions, in the radio frequency quadrupole (RFQ), demonstrating good performance. This article is an overview about how technical challenges impacted the prototype RFPS design and its functional evolution during commissioning, cavity conditioning, and beam operation of the RFQ.
- 17 August 2021
- Published by Institute of Electrical and Electronics Engineers (IEEE) in IEEE Transactions on Plasma Science
- Vol. 49 (9) , 2987-2996
Functional Overview of the RF Power System for the LIPAc RFQ
Design, development, manufacturing, and test activities of the RF power system (RFPS) for Linear IFMIF Prototype Accelerator (LIPAc) were completed in Europe. Installation and commissioning activities were carried out at the International Fusion Materials Irradiation Facility-Engineering Validation and Engineering Design Activities (IFMIF/EVEDA) site in Rokkasho, Japan. Challenging IFMIF requirements led to a number of innovations during design and development. Commissioning required a major effort on calibration and fine setting and led to development of new functionalities. The RFPS was validated under full power and 125-mA deuteron beam loading conditions, in the radio frequency quadrupole (RFQ), demonstrating good performance. This article is an overview about how technical challenges impacted the prototype RFPS design and its functional evolution during commissioning, cavity conditioning, and beam operation of the RFQ.
- 21 April 2020
- Published by Institute of Electrical and Electronics Engineers (IEEE) in IEEE Transactions on Plasma Science
- Vol. 48 (6) , 1489-1495
Integration of 175-MHz LIPAc RF System and RFQ Linac for Beam Commissioning
The eight-chain RF system and radio frequency quadrupole (RFQ) linac were successfully integrated at the facility of the Linear IFMIF Prototype Accelerator (LIPAc). We achieved an unprecedented high current deuteron beam up to 55 mA in pulse operation (300 μs, 1 Hz). The keys of the success were (1) understanding reflected power from RFQ to RF system, (2) tuning each RF chain individually, (3) intensive RF conditioning for holding the stable RF power in the RFQ, and (4) optimizing the beam loading compensation control. Interestingly, the reflection at the breakdown in RF conditioning was higher than an estimation and reached up to 600 kW so far. In order to avoid damage on tetrodes by the high reflection, the impedance of each circulator was accurately adjusted.
- 21 April 2020
- Published by Institute of Electrical and Electronics Engineers (IEEE) in IEEE Transactions on Plasma Science
- Vol. 48 (6) , 1489-1495
Integration of 175-MHz LIPAc RF System and RFQ Linac for Beam Commissioning
The eight-chain RF system and radio frequency quadrupole (RFQ) linac were successfully integrated at the facility of the Linear IFMIF Prototype Accelerator (LIPAc). We achieved an unprecedented high current deuteron beam up to 55 mA in pulse operation (300 μs, 1 Hz). The keys of the success were (1) understanding reflected power from RFQ to RF system, (2) tuning each RF chain individually, (3) intensive RF conditioning for holding the stable RF power in the RFQ, and (4) optimizing the beam loading compensation control. Interestingly, the reflection at the breakdown in RF conditioning was higher than an estimation and reached up to 600 kW so far. In order to avoid damage on tetrodes by the high reflection, the impedance of each circulator was accurately adjusted.