Naoji Yamamoto | Last modified dateļ¼2023.09.26 |
Professor /
Engineering Science for Advanced energy system /
Department of Advanced Energy Science and Engineering /
Faculty of Engineering Sciences
Presentations
1. | Naoji Yamamoto, Kohei Takase, Akira kakami, Yuya Hirano, Kimiya Komurasaki, Ryudo Tsukizaki, Satoshi Hosoda, Hitoshi Kuninaka, Shigeru Yokota, Thrust Performance in a 5 kW Class Anode Layer Type Hall Thruster, 34th IEPC/30th ISTS, 2015.07, [URL]. |
2. | Naoji Yamamoto, Haruki Takegahara, Hiroki Watanabe, Kyoichi Kuriki, Taichiro Tamida, Hiroyuki Osuga, Thrust Performance in Hall Thruster with Pulsating Operation, 34th IEPC/30th ISTS, 2015.07, [URL]. |
3. | Naoji Yamamoto, Plasma-materials interactions in spacecraft propulsion, Plasma conference 2014, 2014.11. |
4. | Naoji Yamamoto, kibe atsushi, Hideki Nakashima, Erosion Sensor for Anode Layer Type Hall Thruster,, 29th International Symposium on Space Technology and Science,, 2013.06. |
5. | Naoji Yamamoto, Development of a miniature microwave discharge neutralizer for miniature ion engines, 33rd International Electric Propulsion Conference, 2013.10. |
6. | Naoji Yamamoto, et al., Developments of Robust Anode-layer Intelligent Thruster for Japan IN-space propulsion system, 33rd International Electric Propulsion Conference, 2013.10. |
7. | Naoji Yamamoto, H. Takegahara, H. Osuga, K. KUriki, T. tamida, J. Aoyagi, Development of a novel power processing unit for Hall thrusters, , IEPC2013, 33rd International Electric Propulsion Conference, 2013.10. |
8. | Naoji Yamamoto, Hideki Nakashima, Azer P.Yalin, Dependence of lifetime on magnetic field configuration in a Hall thruster, 48th AIAA/ASME/SAE/ASEE Joint Propulsion Conference & Exhibit,, 2012.07. |
9. | Development of Microwave Discharge Ion Engine by using Monopole. |
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