Kyushu University Academic Staff Educational and Research Activities Database
List of Papers
Naoji Yamamoto Last modified date:2017.05.06

Professor / Engineering Science for Advanced energy system / Department of Advanced Energy Science and Engineering / Faculty of Engineering Sciences


Papers
1. Naoji Yamamoto, Kohei Takase, Yuya Hirano, Kimiya Komurasaki, Akira Kakami, Ryudo Tsukizaki, Satoshi Hosoda, Hitoshi Kuninaka, Shigeru Yokota, Thrust Performance in a 5 kW Class Anode Layer Type Hall Thruster, Transactions of the Japan Society for Aeronautical and Space Sciences, Aerospace Technology Japan, 14, No. ists30 (ISTS Special Issue: Selected papers from the 30th International Symposium on Space Technology and Science), 2017.02.
2. Koichi Ushio, Yuji Toyoda, Naoji Yamamoto, Taichi Morita, Hideki Nakashima, Development of a Miniature Microwave Discharge Thruster, Transactions of Japan Society for Aeronautical and Space Sciences, Space Technology Japan,, 14, 2016.12.
3. Naoji Yamamoto, Takumi Ito, Haruki Takegahara, Hiroki Watanabe, Taichiro Tamida, Hiroyuki Osuga, Thrust Performance in Hall Thruster with Pulsating Operation, Transactions of the Japan Society for Aeronautical and Space Sciences, Aerospace Technology Japan, 14, No. ists30 (ISTS Special Issue: Selected papers from the 30th International Symposium on Space Technology and Science), 2016.12.
4. Naoji Yamamoto, Atsushi Yamaguchi, Atsushi Kibe, Taichi Morita, Hideki Nakashima, Measurement of Aluminum Erosion Rate by Cavity Ring-Down Spectroscopy, Transactions of the Japan Society for Aeronautical and Space Sciences, Aerospace Technology Japan, 14, No. ists30 (ISTS Special Issue: Selected papers from the 30th International Symposium on Space Technology and Science), 2016.11.
5. Naoji Yamamoto, Hideki Nakashima, Yushi Maeda, Hiroki Watanabe, Ikkoh Funaki, Investigation of Erosion and Deposition in a Microwave Discharge Neutralizer, Transactions of the Japan Society for Aeronautical and Space Sciences, 59, No. 2, 2016.03.
6. Ryosuke Kawashima, Taichi Morita, Naoji Yamamoto, Naoya Saito, Shinsuke FUJIOKA,, H. Nishimura, H. Matsukuma, Atsushi SUNAHARA, Yoshitaka MORI,, Tomoyuki JOHZAKI, Hideki Nakashima, The Measurement of Plasma Structure in a Magnetic Thrust Chamber, Plasma and Fusion Research, 11, 2016.02.
7. Atsushi Yamaguchi, Atsushi Kibe, Naoji Yamamoto, Taichi Morita, Hideki Nakashima, Masakatsu Nakano, Erosion rate measurement in ion thrusters using Cavity Ring-Down Spectroscopy technique, JOURNAL OF INSTRUMENTATION, 11, 2016.01.
8. Naoya Saito, Hiroshi Tominaga, Ryosuke Kawashima, Taichi Morita, Naoji Yamamoto, Hideki Nakashima, Shinsuke FUJIOKA,, Atsushi SUNAHARA, Yoshitaka MORI,, Tomoyuki JOHZAKI, Acceleration of Miniature Targets by Kilo-Tesla Magnetic Field, TRANSACTIONS OF THE JAPAN SOCIETY FOR AERONAUTICAL AND SPACE SCIENCES, AEROSPACE TECHNOLOGY JAPAN, 13, 2015.06.
9. T. Tamida, H. Osuga, Naoji Yamamoto, H. Takegahara,, J. Aoyagi, K. Kuriki, Performance Improvement of Hall Thrusters Using a Pulse-Synchronous Driver System, Journal of Propulsion and Power, Vol. 31, No. 3 (2015), pp. 956-961. , 31, 3, 2015.05.
10. Naoji Yamamoto, H. Takegahara,, J. Aoyagi, K. Kuriki, T. Tamida, H. Osuga, Development of a novel power processing unit for Hall thrusters, IEEE TRANSACTIONS ON PLASMA SCIENCE,, 41, 1, 2015.01.
11. Keisuke TANAKA, Ryosuke KAWASHIMA, Naoji Yamamoto, Taichi Morita, Hideki Nakashima, Diagnostics of Fireball by Discharge on the Surface of an Electrolyte Floating Particulates, Frontier of Applied Plasma Technology, 8, 1, 2015.01.
12. Indranuj Dey, yuji toyoda, Naoji Yamamoto, Hideki Nakashima, Experimental investigation of microwave interaction with magnetoplasma in miniature multipolar configuration using impedance measurements
, Physics of Plasmas, 21, 9, 093502 , 2014.09.
13. B. C. Lee, W. Huang, L. Tao, Naoji Yamamoto, A. D. Gallimore, A. P. Yalin, A cavity ring-down spectroscopy sensor for real-time Hall thruster erosion measurements, Review of Scientific Instruments, 85, Volume 85 ,053111, 2014.05.
14. I. Dey, Y. Toyoda, K. Hirano, N. Yamamoto, and H. Nakashima, Development of a Low Power Multipole Confined Microwave Plasma Ion Thruster, Transactions of the Japan Society for Aeronautical and Space Sciences, Aerospace Technology Japan,, 12, No. ists29, Pb_7-Pb_12, (2014.03), 2014.03.
15. A. Maeno, T. Hinaga, N. Yamamoto, A. Sunahara, S. Fujioka, and H. Nakashima, Effect of Magnetic Field Strength on a Magnetic Thrust Chamber System, Journal of Propulsion and Power, 30, 1, pp.54-61, 2014.01.
16. A. Maeno, N. Yamamoto, S. Fujioka, Y. Mori, A. Sunahara, T. Johzaki, and H. Nakashima, Analysis of Laser Wavelength and Energy Dependences of the Impulse in a Magnetic Thrust Chamber System for a Laser Fusion Rocket, Transactions of the Japan Society for Aeronautical and Space Sciences, 56, 3, pp.170-172, 2013.04.
17. Masato Yasunaga, Akihiro Maeno, Naoji Yamamoto, Hideki Nakashima, Demonstration Experiment of Magnetic Thrust Chamber for a Laser Fusion Rocket, Transactions of Japan Society for Aeronautical and Space Sciences, Space Technology Japan,, 2013.02.
18. Fujioka, Shinsuke, Zhang, Zhe, Ishihara, Kazuhiro, Shigemori, Keisuke, Hironaka, Youichiro, Johzaki, Tomoyuki, Sunahara, Atsushi, Naoji Yamamoto, Hideki Nakashima, Watanabe, Tsuguhiro, Shiraga, Hiroyuki, Nishimura, Hiroaki, Azechi, Hiroshi, Kilotesla Magnetic Field due to a Capacitor-Coil Target Driven by High Power Laser, SCIENTIFIC REPORTS, 3, 2013.01.
19. Naoji Yamamoto, Yoshiaki Hiraoka, Kensaku Sugita, Tomoaki Kurita, KENTARO TOMITA, Kiichiro Uchino, Hideki Nakashima, Thomson Scattering Diagnostics in the Plasma of an Ion Thruster, Transactions of the Japan Society for Aeronautical and Space Sciences, Aerospace Technology Japan, (ISTS Special Issue: Selected papers from the 28th International Symposium on Space Technology and Science), 10, ists28, 2012.08.
20. Akihiro MAENO, Yoshihiro KAJIMURA, Atsushi SUNAHAR, Naoji Yamamoto, Masato YASUNAG, omoyuki HINAGA, Tomonari HANAYA, Shinsuke FUJIOKA, Tomoyuki JOHZAKI, Yoshitaka MORI, Hideki Nakashima, Numerical Analysis of Magnetic Thrust Chamber System for Laser Fusion Rocket Considering the Creation Process of Laser-Produced Plasma, TRANSACTIONS OF THE JAPAN SOCIETY FOR AERONAUTICAL AND SPACE SCIENCES, AEROSPACE TECHNOLOGY JAPAN, 2012.08.
21. Naoji Yamamoto, KENTARO TOMITA, Kensaku Sugita, Tomoaki Kurita, Hideki Nakashima, Kiichiro Uchino, Measurement of xenon plasma properties in an ion thruster using laser Thomson scattering technique, REVIEW OF SCIENTIFIC INSTRUMENTS, 83, 7, 2012.07.
22. Naoji YAMAMOTO , Toru EZAKI and Hideki NAKASHIMA, Thrust performance of a low power Hall thruster, Transactions of Japan Society for Aeronautical and Space Sciences, Space Technology Japan,, 9, ists28, 2012.05.
23. Hiroyuki OSUGA Fujio KUROKAWA Taichiro TAMIDA Naoji YAMAMOTO, High Efficiency Control Method for the Hall Thruster System through Constant Flow Rate Control by Power Supply Control,, IEICE TRANSACTIONS on Communications, Vol.E95-B, No.1, pp.133-142, 2012.01.
24. N. Yamamoto, L. Tao, A. P. Yalin, Development of Real-time Erosion Monitoring System for Hall Thrusters by Cavity Ring-Down Spectroscopy, Transactions of Japan Society for Aeronautical and Space Sciences, Space Technology Japan,, 8, ists27, pp.Pb_39-Pb_44., 2011.03.
25. T. Ezaki, N. Yamamoto, T. Tsuru, Y. Kotani, H. Nakashima, N. Yamasaki, K. Tomita, and K. Uchino, Plasma Properties in a Miniature Microwave Discharge Ion Thruster, Transactions of Japan Society for Aeronautical and Space Sciences, Space Technology Japan,, 8, ists27, pp.Pb_39-Pb_44., 2011.03.
26. N. Yamamoto, J Shimokawatoko, M. Oya and H. Nakashima, Temperature Measurement in a Radio Frequency Electro-thermal Thruster by Integrated Cavity Output Spectroscopy, Frontier of Applied Plasma Technology, 4, 1, pp.12-15, 2011.01.
27. N Yamamoto, K Tomita, N Yamasaki, T Tsuru, T Ezaki, Y Kotani, K Uchino and H Nakashima, Measurements of electron density and temperature in a miniature microwave discharge ion thruster using laser Thomson scattering technique,and Technology, Plasma Sources Science and Technology, 19, 4, 045009, 2010.06.
28. Tomita Kentaro, Yamamoto Naoji, Yamasaki Naoto, Tsuru Teppei, Uchino Kiichiro, Nakashima Hideki, Thomson-Scattering Diagnostics of Plasmas Produced in Miniature Microwave Discharge Ion Engine, Journal of Propulsion and Power, 26, 2, pp. 381-384, 2010.04.
29. N. Yamamoto, L. Tao,B. Rubin, J.D. Williams and A.P. Yalin, Sputter Erosion Sensor for Anode Layer-Type Hall Thrusters Using Cavity Ring-Down Spectroscopy, Journal of Propulsion and Power, 26, 1, pp.142-148, Vol. 22, pp.925-928,, 2010.01.
30. N. Yamamoto, L. Tao, and A.P. Yalin, Single-mode delivery of 250 nm light using a large mode area photonic crystal fiber, Optics Express, 17, 19, pp.16933-16940, 2009.12, [URL].
31. Naoji YAMAMOTO, Makoto MIYOSHI, Yoshiyuki TAKAO and Hideki NAKASHIMA, Development of a Microwave Discharge Ion Thruster Using Argon, TRANSACTIONS OF THE JAPAN SOCIETY FOR AERONAUTICAL AND SPACE SCIENCES,SPACE TECHNOLOGY JAPAN, 7, ists26, pp.Pb_119-Pb_124, 2009.05.
32. Yoshiyuki TAKAO, Akihiro KUGIMIYA, Shinobu NAGAI, Naoji YAMAMOTO, Yoshihiro KAJIMURA and Hideki NAKASHIMA, Study of 2.5-10cm Size Microwave Discharge Ion Thruster, TRANSACTIONS OF THE JAPAN SOCIETY FOR AERONAUTICAL AND SPACE SCIENCES, SPACE TECHNOLOGY JAPAN, 7, ists26, pp.Pb_155-Pb_158, 2009.05.
33. Naoji YAMAMOTO, Azer P.YALIN, Lei TAO, Timothy B. SMITH, Alec D. GALLIMORE and Yoshihiro ARAKAWA, Development of Real-time Boron Nitride Erosion Monitoring System for Hall Thrusters by Cavity Ring-Down Spectroscopy, TRANSACTIONS OF THE JAPAN SOCIETY FOR AERONAUTICAL AND SPACE SCIENCES,SPACE TECHNOLOGY JAPAN, 7, ists26, pp. pb_1-pb_6, 2009.04.
34. Yamamoto, N., Yalin, A. P., Tao, L., Smith, T. B., Gallimore, A. D. and Arakawa, Y.,, Development of Real-time Boron Nitride Erosion Monitoring System for Hall Thrusters by Cavity Ring-Down Spectroscopy, Transactions of Japan Society for Aeronautical and Space Sciences, Space Technology Japan,, 7, ists26, pp. pb_1-pb_6, 2009.04.
35. Y. Kajimura, T. Kanagawa, N. Yamamoto, H. Nakashima,, Numerical Analysis of the Plasma Behavior in a Miniature Microwave Discharge Ion Thruster, AIP(American Institute of Physics) Conference Proceedings, 2009.01.
36. L. Tao, N. Yamamoto, A.P. Yalin, Cavity Ring-Down Spectroscopy Sensor for Ion Beam Etch Monitoring and End-Point Detection of Multilayer Structures, Review of Scientific Instruments, Volume 79, 115107, 2008.12.
37. Dependence of Thruster Configuration on Thrust Performance in Miniature Ion Thruster.
38. Naoji Yamamoto, Shinya Kondo, Takayuki Chikaoka, Hirokazu Masui and Hideki Nakashima, Effects of Magnetic Field Configuration on Thrust Performance in A Miniature Microwave Discharge Ion Thruster, JOURNAL OF APPLIED PHYSICS., 102, 123304, 2007.12.
39. T.Kanagawa, H.Masui, N.Yamamoto, H.Nakashima, Numerical Analysis for Effect of Magnetic Field Configuration on the Trust Performance in a Miniature Ion Engine, Proc. of the 6th International Symposium on Applied Plasma Science,, Vol. 6, pp.89-92., 2007.09.
40. Masashi Oya, Naoji Yamamoto, Shinji Ogawa, Yoshihiro Kajimura, and Hideki Nakashima, Energy Balance in a Radio Frequency Electrothermal Thruster with Water Propellant, Proc. of the 6th International Symposium on Applied Plasma Science,, Vol. 6, pp.101-105, 2007.09.
41. N. Yamamoto, S. Kondo, T. Kanagawa, T. Chikaoka, K. Yoshihiro, H. Nakashima, Development of Miniature Microwave Discharge Ion Thruster, Proceedings of the VI-th International Workshop on Microwave Discharges: Fundamentals and Applications,, pp.211-215, pp.211-216, 2006.12.
42. Takayuki Chikaoka, Shinya Kondo, Naoji Yamamoto, Hideki Nakashima, Yoshiyuki Takao,, Magnetic Field Configuration Effects on Thrust Performance of Miniature Microwave Discharge Ion Engine, Proc. of the 25th Int. Symposium on Space Technology and Science, pp. 254-258, pp. 254-259, 2006.12.
43. Yoshiyuki Takao, Hiroshi Kataharada, Takashi Miyamoto, Hirokazu Masui, Naoji Yamamoto and Hideki Nakashima,, Performance Test of Micro Ion Thruster using Microwave Discharge,, Vacuum, 80, 11月12日, pp. 1239-1243, Volume 80, Issues 11-12, Pages 1239-1243,, 2006.09.
44. H. Masui, Y. Tashiro, N. Yamamoto, H. Nakashima, I. Funaki, Analysis of Electron and Microwave Behaviors in Microwave Discharge Neutralizer,, Trans. Jpn. Society for Aeronautical and Space Sciences,, Vol.49, No.164, pp.87-93,, 2006.08.
45. N. Yamamoto, H. Masui, H. Kataharada, H. Nakashima, Y. Takao,, Antenna Configuration Effects on Thrust Performance of Miniature Microwave Discharge Ion Engine, J. Propulsion and Power,, Vol. 22, pp.925-928,, 2006.07.
46. H. Kataharada, Y. Takao, N. Yamamoto, H. Ijiri, H. Nakashima, Development of Small Microwave Discharge Ion Thruster, Thin Solid Films, Vol.506-507, pp.605-608,, 2006.03.
47. Naoji YAMAMOTO, Shigeru YOKOTA, Keiko WATANABE, Akihiro SASOH, Kimiya KOMURASAKI, Yoshihiro ARAKAWA, Suppression of Discharge Current Oscillations in a Hall Thruster, Transactions of The Japan Society for Aeronautical and Space Sciences, 48, 161, Vol.48 No.161,, 2005.11.
48. Naoji Yamamoto, Kimiya Komurasaki and Yoshihiro Arakawa, Discharge Current Oscillation in Hall Thrusters, JOURNAL OF PROPULSION AND POWER, 21, 5, Vol.21, No.5, september-October, 2005, pp.870-876, 2005.09.
49. Naoji Yamamoto, Shigeru Yokota, Makoto Matsui and Kimiya Komurasaki,Yoshihiro Arakawa, MEASUREMENT OF EROSION RATE BY ABSORPTION SPECTROSCOPY IN A HALL THRUSTER, Review of Scientific Instruments, 76, 8, Volume 76, Issue 8, 083111, 2005.08.
50. Y. Takao, T. Miyamoto, H. Kataharada, H. Nakashima, H. Masui, T. Kai, H. Ijiri, Y. Mori, N. Yamamoto,, Development of Small-Scale Ion Thruster Utilizing Microwave Discharge Plasma, Proc. of the 24th Int. Symposium on Space Technology and Science,, pp.161-165, pp.161-166, 2004.12.
51. T. Miyamoto, N. Yamamoto, H. Ijiri, Y. Takao, H. Nakashima, Development of a Microwave Discharge Ion Engine by Using Monopole Antennas,, Proc. of the 24th Int. Symposium on Space Technology and Science, pp.137-141, pp.137-142, 2004.12.
52. N. Yamamoto, K. Watanabe, A. Sasoh, K. Komurasaki, Y. Arakawa, Control of Discharge Current Oscillations in Hall Thrusters, Proc. of the 24th Int. Symposium on Space Technology and Science,, pp. 191 -195, pp. 191 -196, 2004.12.
53. Number Density Measurement of Oxygen Atoms in a Hall-Type Ion Source
Plume

Naoji YAMAMOTO, Takafumi NAKAGAWA, Makoto MATSUI, Kimiya KOMURASAKI
and Yoshihiro ARAKAWA.
54. Experimental Investigation of a Hall Thruster using Oxygen as the propellant

Takafumi NAKAGAWA, Naoji YAMAMOTO, Makoto MATSUI, Kimiya KOMURASAKI
and Yoshihiro ARAKAWA.
55. Operating Characteristics of an Anode Layer Type Hall Thruster.
56. Ion Beam Characteristics in Hall Accelerators Using Oxygen Gas

Naoji YAMAMOTO, Takafumi NAKAGAWA, Kimiya KOMURASAKI and Yoshihiro ARAKAWA.
57. Yamamoto N., Nakagawa T., Komurasaki K. and Arakawa Y.,, Effect of Discharge Oscillations on Hall Thruster Performance, Proceedings of the 23rd International Symposium on Space Technology and Science,, pp.319-324, 2002.10.
58. Yamamoto N., Nakagawa T., Komurasaki K. and Arakawa Y.,, Discharge Plasma Fluctuations in Hall Thrusters, Vacuum,, Vol.65,
issues 3-4, (2002), pp. 375-381, 2002.05.
59. Relation between Discharge Oscillations and Performance in Hall Accelerators

Naoji YAMAMOTO, Takafumi NAKAGAWA, Kimiya KOMURASAKI, and Yoshihiro ARAKAWA.
60. Yamamoto N., Nakagawa T., Komurasaki K. and Arakawa Y.,, Observation of Plasma Fluctuations in Hall Accelerators, Proceedings of the 3rd International Symposium on Applied Plasma Science, Advances in Applied Plasma Science, Vol. 3, (2001), pp.95-100, 2001.07.
61. Discharge Oscillations in Hall Thrusters

Naoji Yamamoto, Kimiya Komurasaki, and Yoshihiro Arakawa.
62. Yamamoto N., Momo, S, Komurasaki K. and Arakawa Y.,, Discharge-current Oscillations in Hall Thrusters, Proceedings of the 22nd International Symposium on Space Technology and Science, pp.349-353, pp.349-354, 2000.10.