Published Papers |
No. | Title | Journal | Vol | No | Start Page | End Page | Publication date | DOI | Referee |
1 | Design of a Dorne-mounted Pollinator Sprayer | Journal of Japan Society for Design Engineering | | | | | Apr. 2025 | | Refereed |
2 | Residual vibration control of artificial pollination sprayer for onboard drones  | Mechanical Engineering Letters | 11 | | 25 | 00031 | 2025 | https://doi.org/10.1299/mel.25-000311 | |
3 | Development of an optical and near-infrared telescope onboard the HiZ-GUNDAM mission | Space Telescopes and Instrumentation 2024: Optical, Infrared, and Millimeter Wave | 11444 | | 86 | 86 | Aug. 23, 2024 | https://doi.org/10.1117/12.30135971 | |
4 | High-z gamma-ray bursts unraveling the dark ages and extreme space-time mission - HiZ-GUNDAM | Space Telescopes and Instrumentation 2024: Ultraviolet to Gamma Ray | 736:7 | | 75 | 75 | Aug. 21, 2024 | https://doi.org/10.1117/12.30185711 | |
5 | Surface Degradation of Cable-Mesh Reflector with Pillow Deformation | Journal of Evolving Space Activities | 2 | 155 | | | Aug. 2024 | https://doi.org/10.57350/jesa.1551 | Refereed |
6 | Design and Rigidity Estimation of an Ultra-lightweight Solar Array | Journal of Evolving Space Activities | 1 | 39 | | | Apr. 2023 | https://doi.org/10.57350/jesa.391 | Refereed |
7 | Modeling and Evaluation of Inflatable Tubes for Gravity Compensator of Space Deployable Structures | 設計工学(Web) | 56 | 7 | 341 | 352 | Jun. 2021 | | |
8 | Proposal of a New Concept for Lightweight Solar Array Structures with High Rigidity  | TRANSACTIONS OF THE JAPAN SOCIETY FOR AERONAUTICAL AND SPACE SCIENCES, AEROSPACE TECHNOLOGY JAPAN | 19 | 2 | 144 | 149 | Mar. 2021 | https://doi.org/10.2322/tastj.19.1441 | |
9 | Modeling and Evaluation of Inflatable Tubes for Gravity Compensator of Space Deployable Structures | JOURNAL OF JAPAN SOCIETY FOR DESIGN ENGINEERING | 56 | 7 | 331 | 342 | 2021 | https://doi.org/10.14953/jjsde.2020.29091 | |
10 | Development of an optical and near-infrared telescope onboard the HiZ-GUNDAM mission | Space Telescopes and Instrumentation 2020: Optical, Infrared, and Millimeter Wave | | | | | Dec. 13, 2020 | https://doi.org/10.1117/12.25606541 | |
11 | Experimental Evaluation of Reducing Cable-strain Energy of Tension-truss Surface with compression members | Journal of Spacecraft and Rockets | 57 | 4 | 835 | 843 | Jul. 2020 | | Refereed |
12 | Surface design method incorporating compression members for cable-mesh reflectors | Journal of Spacecraft and Rockets | 55 | 1 | 214 | 222 | 2018 | https://doi.org/10.2514/1.A338751 | Refereed |
13 | Progress in and Prospects of On-Board Communication Equipment Technologies for Communications Satellites in Japan | IEICE TRANSACTIONS ON COMMUNICATIONS | E100B | 9 | 1633 | 1643 | Sep. 2017 | https://doi.org/10.1587/transcom.2016PFI00021 | Refereed |
14 | Technology Trends for Communication Satellite Antenna Systems  | The Journal of the Institute of Electrical Engineers of Japan | 137 | 3 | 166 | 169 | Mar. 2017 | https://doi.org/10.1541/ieejjournal.137.1661 | Not refereed |
15 | Fundamental Design method of Antenna surface including compression members  | The Proceedings of Mechanical Engineering Congress, Japan | 2017 | | G1900101 | | 2017 | https://doi.org/10.1299/jsmemecj.2017.g19001011 | Not refereed |
16 | Design Method for Large Deployable Antenna to Study on Topology of Cable Network  | The Proceedings of the Space Engineering Conference | 2017.26 | | 2A5 | | 2017 | https://doi.org/10.1299/jsmesec.2017.26.2a51 | Not refereed |
17 | Design method of cable network including compression member for large deployable antenna | Transactions of the JSME (in Japanese) | 082 | 843 | 16 | 00162-16-00162 | Nov. 2016 | https://doi.org/10.1299/transjsme.16-001621 | Refereed |
18 | Preliminary research of design procedure for space deployable structures with surfaces of revolution composed of scissors members  | The Proceedings of the Space Engineering Conference | 2016.25 | | 2A3 | | 2016 | https://doi.org/10.1299/jsmesec.2016.25.2a31 | Not refereed |
19 | J1910101 Conceptual Study of Lightweight Structures for Concentrator Photovoltaic System  | The Proceedings of Mechanical Engineering Congress, Japan | 2014 | | _J1910101- | _J1910101- | 2014 | https://doi.org/10.1299/jsmemecj.2014._j1910101-1 | Not refereed |
20 | P09 Fundamental Research of Relative Motion in Positioning Mechanism Using Kinematic Couplings  | The Proceedings of the Space Engineering Conference | 2013.22 | | _P09-1_ | _P09-3_ | 2013 | https://doi.org/10.1299/jsmesec.2013.22._p09-1_1 | Not refereed |
21 | An 80-kWh-class telecommunications backup system with large-scale nickel metal hydride batteries | World Telecommunications Congress 2010, WTC 2010 | | | 22 | 24 | 2010 | | |
22 | Thermal behavior of a weatherproof power supply system with built-in nickel-metal hydride batteries developed for stationary use | JOURNAL OF POWER SOURCES | 194 | 2 | 1156 | 1163 | Dec. 2009 | https://doi.org/10.1016/j.jpowsour.2009.06.0141 | Refereed |
23 | An air-breathing single cell small proton exchange membrane fuel cell system with AB5-type metal hydride and an ultra-low voltage input boost converter | JOURNAL OF POWER SOURCES | 186 | 1 | 37 | 44 | Jan. 2009 | https://doi.org/10.1016/j.jpowsour.2008.09.0511 | Refereed |
24 | Outdoor power-supply system | NTT Technical Review | 6 | 2 | | | Feb. 2008 | | |
25 | Charge/discharge characteristics of a backup power supply system using nickel metal hydride batteries | INTELEC 07 - 29TH INTERNATIONAL TELECOMMUNICATIONS ENERGY CONFERENCE, VOLS 1 AND 2 | | | 614 | 620 | 2007 | | Refereed |
26 | Reduction of Heat Generation from Onboard SSPA by Using Heat Suppression Signal  | JOURNAL OF THE JAPAN SOCIETY FOR AERONAUTICAL AND SPACE SCIENCES | 52 | 610 | 507 | 513 | Nov. 2005 | https://doi.org/10.2322/jjsass.52.5071 | Refereed |
27 | Heat Suppressing Technique for Onboard Amplifiers by Hub Station Control  | The IEICE transactions on communications B | J88-B | 1 | 193 | 196 | Jan. 2005 | | Refereed |
28 | Experimental Estimation for Thermal Control of Onboard Battery during Charging at the Launch Site  | JOURNAL OF THE JAPAN SOCIETY FOR AERONAUTICAL AND SPACE SCIENCES | 52 | 602 | 121 | 128 | Mar. 2004 | https://doi.org/10.2322/jjsass.52.1211 | Refereed |
29 | Visual analysis in a deployable antenna experiment | IEEE TRANSACTIONS ON AEROSPACE AND ELECTRONIC SYSTEMS | 40 | 1 | 247 | 258 | Jan. 2004 | https://doi.org/10.1109/TAES.2004.12921571 | Refereed |
30 | A Deploying Process Analysis Using Sub-Pixel Cross-Correlation Method : An Application for Deploying Experiment of Small-Scaled Model of ETS-VIII Deployable Antenna  | JOURNAL OF THE JAPAN SOCIETY FOR AERONAUTICAL AND SPACE SCIENCES | 50 | 587 | 496 | 503 | Dec. 2002 | https://doi.org/10.2322/jjsass.50.4961 | Refereed |
31 | Development of Loop Heat Pipe deployable radiator for use on Engineering Test Satellite VIII (ETS-VIII) | SAE Technical Papers | | | | | 2001 | https://doi.org/10.4271/2001-01-23411 | Refereed |
32 | Mathematical modeling for predicting steady state and transient characteristics of Reservoir Embedded Looped Heat Pipe (RELHP) | SAE Technical Papers | | | | | 2001 | https://doi.org/10.4271/2001-01-22391 | Refereed |
33 | Thermal Distortion of a Modular Structure for Use a Large Reflector  | Transactions of the Japan Society of Mechanical Engineers Series B | 66 | 646-A | 136 | 143 | Jun. 2000 | https://doi.org/10.1299/kikaia.66.12101 | Refereed |
34 | Satellite mesh reflector temperature measured by using fine thermocouples | Journal of Thermophysics and Heat Transfer | 13 | 1 | 164 | 165 | 1999 | https://doi.org/10.2514/2.64181 | Refereed |
35 | Thermal Design Evaluation of Large Reflector Deployment Mechanism by Using Flight Data.  | Aeronautical and Space Sciences Japan | 44 | 508 | 284 | 290 | Aug. 1996 | https://doi.org/10.2322/jjsass1969.44.2841 | Refereed |
36 | A Thermal Design Verification of Large Reflectors Using Flight Data  | Aeronautical and space sciences Japan | 44 | 506 | 190 | 195 | Mar. 1996 | https://doi.org/10.2322/jjsass1969.44.1901 | Refereed |
37 | Deployment mechanism for a large reflector: Thermal-design verification using flight data | Journal of Spacecraft and Rockets | 32 | 5 | 890 | 893 | 1995 | https://doi.org/10.2514/3.267011 | Refereed |
38 | Experimental results for capillary looped pipe applied to direct cooling method | Journal of Thermophysics and Heat Transfer | 9 | 1 | 96 | 100 | 1995 | https://doi.org/10.2514/3.6331 | Refereed |
39 | Thermal design verification of a large deployable antenna for a communications satellite | Journal of Spacecraft and Rockets | 29 | 2 | 271 | 278 | 1992 | https://doi.org/10.2514/3.263451 | Refereed |
40 | Thermal Design Evaluation of On-Board Large Deployable Antenna.  | Aeronautical and Space Sciences Japan | 39 | 453 | 504 | 512 | Oct. 1991 | https://doi.org/10.2322/jjsass1969.39.5041 | Refereed |
41 | Thermal Design verification of large deployable antenna for ETS-VI | AIAA 26th Thermophysics Conference, 1991 | | | | | 1991 | https://doi.org/10.2514/6.1991-13011 | |
42 | Heat transport performance of axially grooved heat pipe with multiple heating points.  | Aeronautical and Space Sciences Japan | 37 | 424 | 222 | 227 | May. 1989 | https://doi.org/10.2322/jjsass1969.37.2221 | Refereed |
MISC |
No. | Title | Journal | Vol | No | Start Page | End Page | Publication date |
1 | Surface Potential History and Volume Resistivity of Polyimide Film at Cryogenic Temperature  | 宇宙航空研究開発機構特別資料: 第14回「宇宙環境シンポジウム」講演論文集 = JAXA Special Publication: Proceedings of the 14th Spacecraft Environment Symposium | | 17 | 169 | 173 | Jan. 15, 2018 |
2 | Experimental verification of weight reduction effect for cable network with compression members | 宇宙科学技術連合講演会講演集(CD-ROM) | 62nd | | | | 2018 |
3 | Charging Characteristics of Spacecraft Dielectric Material at Cryogenic Temperature  | 宇宙航空研究開発機構特別資料: 第13回宇宙環境シンポジウム講演論文集 = JAXA Special Publication: Proceedings of the 13th Spacecraft Environment Symposium | | 16 | 145 | 148 | Feb. 15, 2017 |
4 | D04 Design method of cable network including compression member for large deployable antenna | | 2015 | 24 | "D04 | 1"-"D04-4" | Dec. 21, 2015 |
5 | Characteristics of Pneumatic Gravity Compensation System Applied to Three-dimensional Movement of Deployable Structures  | | 58 | | 4p | | Nov. 12, 2014 |
6 | A Study on a structural characteristic of a cable network structure integrated with compression members for accurate large antenna  | | 58 | | 4p | | Nov. 12, 2014 |
7 | J1910103 The study on internal pressure character of a gravity compensation device underpinning deploy able space structures | Mechanical Engineering Congress, Japan | 2014 | | "J1910103 | 1"-"J1910103-3" | Sep. 7, 2014 |
8 | B03 Optimum Design of Supporting Structure of Cable-Mesh Antenna Reflector | | 2013 | 22 | "B03 | 1"-"B03-5" | Dec. 20, 2013 |
9 | B04 A Study on Buckling Analysis of Joint for Flexible Multibody Structures | | 2013 | 22 | "B04 | 1"-"B04-4" | Dec. 20, 2013 |
10 | Technical approaches to clean-energy power systems | NTT Technical Review | 4 | 3 | 37 | 41 | Mar. 2006 |
11 | B2 The Design of Large Deployable Reflector for ETS-VIII | | | | 35 | 41 | 2001 |
12 | STRUCTURAL DESIGN COORDINATING THERMAL ESTIMATION FOR LARGE DEPLOYABLE REFLECTOR  | Proceedings of the conference on computational engineering and science | 2 | 2 | 537 | 540 | May. 28, 1997 |
13 | Estimation of the maximum RF power using the acceptance temperature and the efficiency for phased array feeder | Technical report of IEICE. SAT | 96 | 316 | 15 | 22 | Oct. 18, 1996 |
14 | Heat-Transport Characteristics of Capillary Looped Pipes  | Transactions of the Japan Society of Mechanical Engineers. Series B. | 61 | 582 | 665 | 671 | Feb. 25, 1995 |
Conference Activities & Talks |
No. | Title | Conference | Publication date | Promoter | Venue |
1 | Pillow Deformation of Cable-mesh Surface Antenna | The 34th International Symposium on Space Technology and Science, | Jun. 6, 2023 | | |
2 | Compensator in Large Deployable Structure for Space Using Mecanum Wheel | The 34th International Symposium on Space Technology and Science, | Jun. 6, 2023 | | |
3 | Design of Solar Paddle With Improved Power Generation Using Multiple Reflections | The 34th International Symposium on Space Technology and Science | Jun. 6, 2023 | | |
4 | Antenna Structural Concept Composed of Scissors Member Connected with Convex Tapes | The 34th International Symposium on Space Technology and Science, | Jun. 6, 2023 | | |
5 | Scissors-Structure Antenna Design on Initial Deployment Force Generated by Strain Energy | 33rd International Symposium on Space Technology and Science | Mar. 2, 2022 | | |
6 | Cable-Mesh Surface Design for Large Antenna Including Mesh Deformation | 33rd International Symposium on Space Technology and Science | Mar. 2, 2022 | | |
7 | Vibration characteristics of ultra-lightweight with high-rigidity solar array structure | 33rd International Symposium on Space Technology and Science | Mar. 2, 2022 | | |
8 | Fundamental Design Method of Antenna Surface Including Compression Members | 31st International Symposium on Space Technology and Scient | Jun. 2017 | | |
9 | Preliminary Design Study on Tension Truss Antenna Surface for Shape Stability | 31st International Symposium on Space Technology and Scient | Jun. 2017 | | |
10 | Preliminary Study of Deployable Structures Assembled with Scissors Members Applied for Parabolic Reflectors | 31st International Symposium on Space Technology and Scient | Jun. 2017 | | |
11 | Fundamental Study on Vibration Characteristics of Space Solar Power Systems | 31st International Symposium on Space Technology and Scient | Jun. 2017 | | |
12 | Preliminary Investigations of Pneumatic Gravity Compensation System for Deployable Space Structures | 31st International Symposium on Space Technology and Scient | Jun. 2017 | | |
13 | High-Precision Positioning of Flexible deployable Structures Using Kinematic Couplings | 46th international conference on environmental systems ICES 2016 | Oct. 2015 | | |
14 | Estimation of thermal distortion of reflector formed by truss structure | 30th International Symposium on Space and Technology and Sicence | Jul. 2015 | | |
15 | Pneumatic gravity compansation system applied to three-dimensional movement of deployable structure | 30th International Symposium on Space and Technology and Sicence | Jul. 2015 | | |
16 | An 80-kWh-class Telecommunications Backup System with Large-scale Nickel Metal Hydride Batteries | Telecommunications: The Infrastructure for the 21st Century (WTC) | Sep. 2010 | | |
17 | Artificial Neural Network for State-of-Charge Estimation of a Ni-MH Battery with a Photovoltaic Power System | 216th ECS Meeting | Oct. 2009 | | |
18 | Low-current Charge Properties of Large-scale Nickel Metal Hydride Batteries and Application to Photovoltaic Power Generation | 214th meeting of ECS | Oct. 2009 | | |
19 | Charge/discharge characteristics of a backup power supply system using nickel metal hydride batteries | Telecommunications energy conference | Sep. 2007 | | |
20 | Integration and Testing of Large Deployable Reflector on ETS-VIII | AIAA ICSSC-21 | Apr. 2003 | | |
21 | Performances D’un Reflecteur De La Taille D’un Court De Tennis Pour ETS-VIII | 12èmes Journées Internationales de Nice sur les Antennes International Symposium on Antennas | Nov. 2002 | | |
22 | A Tennis-court-sized Reflector for Communication Satellites | 2002 Joint Conference on Satellite Communications, JC-Sat 2000 | Oct. 2002 | | |
23 | Ground verification Methods for Surface Accuracy of Large Deployable Antenna Reflector | 23rd International Symposium on Space Technology and Science | May. 2002 | | |
24 | Mathematical Modeling for Predicting Steady State and Transient Characteristics of Reservoir Embedded Looped Heat Pip | 31st International Conference on Environmental Systems Proceedings | Jul. 2001 | | |
25 | Development of Loop Heat Pipe Deployable Radiator for Use on Engineering Test Satellite VIII | 31st International Conference on Environmental Systems Proceedings | Jul. 2001 | | |
26 | Design and Ground Verification of Large Deployable Antenna | 42nd AIAA/ASME/AHS/ASC Structural Dynamics & Material | Apr. 2001 | | |
27 | Analysis and Test Methods for Large Deployable Space Structure | 42nd AIAA/ASME/AHS/ASC Structural Dynamics & Material | Apr. 2001 | | |
28 | Thermal Balance Testing for A Large Deployable Reflector | 29th International Conference on Environmental Systems Proceedings | Jan. 1999 | | |
29 | Development of a 15 m Class Modular Mesh Deployable Antenna | 48th International Astronautical Congress | Oct. 1997 | | |
30 | Thermal Distortion of Over 10 Meter Diameter Reflectors Formed by Truss Structure | AIAA 32nd Thermophysics Conference | Jun. 1997 | | |