Kyushu University Academic Staff Educational and Research Activities Database
List Of Papers
Last modified date：2012.5.7
Hideki Nakashima
Professor
energy system sicence
Department of Engineering Science
Faculty of Engineering Sciences

Papers

1. Naoji YAMAMOTO, Kentaro TOMITA, Tomoaki KURITA, Kiichiro UCHINO, and Hideki NAKASHIMA,Thomson Scattering Diagnostics in the Plasma of an Ion Thruster,Transactions of the Japan Society for Aeronautical and Space Sciences, Space Technology Japan,Vol.9,2012.04.
2. Naoji YAMAMOTO , Toru EZAKI and Hideki NAKASHIMA,Thrust performance of a low power Hall thruster,Transactions of the Japan Society for Aeronautical and Space Sciences, Space Technology Japan,Vol.9,2012.04.
3. 鷹尾良行，山本直嗣，中島秀紀,口径3cmおよび5cm級マイクロ波放電型イオンエンジンの開発,Applied Plasma Science,Vol.18,No.2,pp. pp.182-186,2010.09.
4. Y. Kajimura, I. Funaki, H. Nishida, H. Usui, I. Shinohara, H. Yamanaka, H. Nakashima,Quantitative Evaluation of Ion Kinetic Effect in Magnetic Field Inflation by the Injection of a Plasma Jet,Trans. Japan Soc. Aero. Space Sci.,Vol.54,No.184,pp. pp.90-97,2011.09.
5. Y. Kajimura, T. Norimastu, H. Nakashima,Numerical Study for Laser Source Protection from Alpha Particles by Magnetic Fields in a Laser Fusion Reactor,Plasma and Fusion Research,Vol.6,pp. 2404049,2011.09.
6. Y. Kajimura, H. Nakashima,Verification of Hybrid Particle-in-Cell Simulation Model for Advanced Plasma Propulsions: Magento Plasma Sail and Magnetic Nozzle for Laser Fusion Rocket,J. Space Technology and Science,Vol.25,No.2,pp. pp.34-54,2011.09.
7. A. Maeno, N. Yamamoto, H. Nakashima, S. Fujioka, A. Sunahara, T. Johzaki, Y. Mori,Direct Measurement of the Impulse in a Magnetic Thrust Chamber System for Laser Fusion Rocket,Applied Physics Letters,Vol.99,No.7,pp. 071501,2011.08.
8. Naoji YAMAMOTO, Jun SHIMOKAWATOKO, Masashi OYA and Hideki NAKASHIMA,Temperature Measurement in a Radio Frequency Electro-thermal Thruster by Integrated Cavity Output Spectroscopy,Frontier of Applied Plasma Technology,Vol.4,No.1,2011.03.
9. K. Tomita, N. Yamamoto, N. Yamasaki, T. Tsuru, K. Uchino, H. Nakashima,Thomson-Scattering Diagnostics of Plasmas Produced in Miniature Microwave Discharge Ion Engine,Journal of Propulsion and Power,Vol.26,pp. pp.381-384,2010.03.
10. 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,Plasma Sources Science and Technology,Vol.19,045009.,2010.09.
11. T.NISHIYAMA, H.NAGATA, H.NAKASHIMA,Proposal of Space Reactor for Nuclear Electric Propulsion System,2009 International Congress on Advances in Nuclear Power Plants,2009.05.
12. Toru Ezaki, Naoji Yamamoto, Teppei Tsuru, Usuke Kotani, Hideki Nakashima, Naoto Yamasaki, Kentaro Tomita, Kiichiro Uchino,Plasma Properties in a Miniature Microwave Discharge Ion Thruster,TRANSACTIONS OF THE JAPAN SOCIETY FOR AERONAUTICAL AND SPACE SCIENCES, AEROSPACE TECHNOLOGY JAPAN,2011.03.
13. Teppei TSURU, Shinya KONDO, Naoji YAMAMOTO, and Hideki NAKASHIM,Development of Miniature Microwave Discharge Neutralizer,Selected papers from the 26th International
Symposium on Space Technology and Science, Transactions of Japan Society
for Aeronautical and Space Sciences, Space Technology ,Vol.Vol.7,ISTS2008-b-35,2010.04.
14. Akihiro Maeno, Hanaya Tomonari, Hideki Nakashima, Shinsuke Fujioka, Atsushi Sunahara, Tomoyuki Johzaki, Yoshitaka Mori,Magnetic Thrust Chamber Propulsion System for Controlling Laser-Produced Plasma by Magnetic Fields,TRANSACTIONS OF THE JAPAN SOCIETY FOR AERONAUTICAL AND SPACE SCIENCES, SPACE TECHNOLOGY JAPAN, ISTS Special Issue: Selected papers from the 27th International Symposium on Space Technology and Science., 2009-b-37,2010.03.
15. M. OYA, N. YAMAMOTO, H. NAKASHIMA,Energy Balance in a Radio Frequency Electro-thermal Thruster ,Proc. 31st International Electric Propulsion Conference,2009.09.
16. Akihiro Maeno, Hanaya Tomonari, Naoji Yamamoto, Hideki Nakashima, Shinsuke Fujioka, Atsushi Sunahara, Tomoyuki Johzaki, Yoshitaka Mori,Preliminary Experiments for Demonstrating Magnetic Nozzle Concept in Laser Fusion Rocket,Proceedings of 31st International Electric Propulsion Conference, IEPC-2009-006,2009.09.
17. Y. Kajimura, H. Usui, M. Nunami, I. Funaki, I. Shinohara, H. Nakashima,,Numerical Study of Inflation of a Dipolar Magnetic Field in Space by Plasma Jet Injection,Journal of Plasma and Fusion Research Series ,Vol.Vol.8,pp.pp.1616-1621,2009.08.
18. Y. Kajimura, R. Kawabuchi, A. Maeno, H. Nakashima, T. Norimatsu,Numerical Study for a Protection of Laser Beam Port by Magnetic Fields in the Laser Fusion Reactor KOYO-F,Journal of Plasma and Fusion Research Series,Vol.Vol.8,pp.pp.1248-1252,2009.08.
19. N. MATSUDA, A. MAENO, Y. KAJIMURA, H. NAKASHIMA,A Magnetic Thrust Chamber Design For A Laser Fusion Rocket Based on Impact Fast Ignition Scheme,Journal of Plasma and Fusion Research Series,Vol.Vol.8,pp.pp.1602-1605,2009.08.
20. 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,Vol.Vol. 7,No.No. ists26 ,pp.pp.Pb_119-Pb_124,2009.07.
21. T. Nishiyama, H. Nagata, H. Nakashima,Proposal of Space Reactor for Nuclear Electric Propulsion System,Proc. Int. Congress on Advances in Nuclear Power Plant,Paper No. 9186,2009.06.
22. H. Nagata, T. Nishiyama , H. Nakashima,Proposal of Space Reactor for Nuclear Electric Propulsion System,Transactions of Japan Society for Aeronautical and Space Sciences, Space Technology Japan,　Vol. 7 (2009)
2008-b-08,2009.05.
23. Y. Kajimura, N. Matsuda, K. Hayashida, A. Maeno, H. Nakashima,Numerical Simulation of Plasma Behavior in a Magnetic Nozzle of a Laser-plasma Driven Nuclear Electric Propulsion System,AIP（American Institute of Physics） Conference Proceedings,Vol. 1084, pp.934-938,2009.01.
24. 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,Vol.Vol. 1084,pp.pp.939-944,2009.01.
25. Y. Takao, A. Kugimiya, S. Nagai, N. Yamamoto, H. Nakashima, A. Kobayashi,Development of Neutralizer by Using CNT for Miniature Ion Engine,Frontier of Applied Plasma Technology,2008.07.
26. N. Matsuda, R. Kawabuchi, Y. Kajimura, H. Nakashima, Y. P. Zakaharov,Improvement of Thrust Efficiency of Laser Fusion Rocket with Shaped Target ,Journal of Physics : Conference Series,,Vol. 112, 042079,2008.06.
27. R Kawabuchi, N Matsuda, Y Kajimura, H Nakashima , Y P Zahaharov ,Numerical Simulation of Plasma Detachment from a Magnetic Nozzle by using Fully Particle-In-Cell Code ,Journal of Physics :IOP Conference Series,Vol. 112, 042082,2008.06.
28. Y. P Zakharov, K V Vchivkov, H Nakashima, E L Boyarintsev,A V Melekhov, V G Posukh, I F Shaikhislamov , Y Kajimura　,Advanced Study of ICF-energy Direct Conversion for Laser Fusion Rocket with Quasi-dipole Field in the Laser-plasma Experiments and PIC–simulations,Journal of Physics : Conference Series,Vo. 112, 042078,2008.06.
29. 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 ,2007,2007.12.
30. T. Kanagawa, N. Yamamoto, Y. Kajimura and H. Nakashima,Numerical Simulation of Internal Plasma in a Miniature Microwave Discharge Ion Thruster,Proc. of the 30th International Electric Propulsion Conference, IEPC-2007-190, 2007.,2007.09.
31. M. Oya, N. Yamamoto, S. Ogawa, Y. Kajimura and H. 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.,2007.09.
32. Y. Kajimura, R. Kawabuchi, N. Matsuda and H. Nakashima,Numerical simulation of fusion plasma behaviors in a magnetic nozzle.,Transactions of Fusion Science and Technology, Vol.51, No.2T, FUSTE8, pp.229-231, 2007.,2007.01.
33. Yoshihiro Kajimura, Kenji Noda, Hideki Nakashima and Ikkoh Funaki,Feasibility Study of Magneto Plasma Sail by Using Numerical Simulation and Experiment.,45th AIAA Aerospace Sciences Meeting and Exhibit AIAA 2007-587 ,2007.01.
34. 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, 2006,2006.10.
35. Y. Kajimura, R. Kawabuchi, N. Matsuda and H. Nakashima,Numerical Simulation of Fusion Plasma Behaviors in a Magnetic Nozzle,Transactions of Fusion Science and Technology (2006) ,2006.10.
36. Naoji Yamamoto, Shinya Kondo, Takayasu Kanagawa, Takayuki Chikaoka, Yoshihiro Kajimura, Hideki Nakashima,DEVELOPMENT OF MINIATURE MICROWAVE DISCHARGE ION THRUSER,VI-th International Workshop on Microwave Discharges: Fundamentals and Applications, September, 2006, pp.211-216,2006.09.
37. Y. Mori, H. Nakashima, F. W. Baity Jr., R. H. Goulding, M. D. Saprks,Focusing Magnetic Field Contribution for Helicon Plasma on Mini-RFTF,Thin Solid Films, Vol.506-507, pp.583-587, 2006,2006.08.
38. H. Masui, , T. Tanoue, H. Nakashima, I. Funaki,Numerical analysis of microwave ion engine using electromagnetic particle code ,Thin Solid Films, Vol.506-507, pp.609-612, 2006,2006.08.
39. 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, 2006,2006.08.
40. Yoshihiro Kajimura, Ryo Kawabuchi and Hideki Nakashima,Control Techniques of Thrust Vector for Magnetic Nozzle in Laser Fusion Rocket,Fusion Engineering and Design 81, pp2871-2875 (2006)　,2006.07.
41. Yoshihiro Kajimura, Daisuke Shinohara, Kenji Noda, Hideki Nakashima,Numerical Simulation of Magneto Plasma Sail by using Three-Dimensional Hybrid Code.,25th International Symposium on Space Technology and Science, ISTS 2006-b-48 ,2006.06.
42. Nobutaka Munesada, Keisuke Shinyashiki, Makoto Miyoshi, Takashi Miyamoto, Naoji Yamamoto, Yoshihiro Kajimura, and Hideki Nakashima,Effects of magnetic field and antenna configurations on thrust performance of microwave discharge ion engines with multi mono pole antenna system,25th Int. Symposium on Space Technology and Science ISTS 2006-b-29,2006.06.
43. Takayuki KASA, Takayasu KANAGAWA, Keisuke IZUMI, Hirokazu MASUI, Naoji YAMAMOTO, Yoshihiro KAJIMURA, Hideki NAKASHIMA,Numerical Analysis of Microwave Discharge Plasma Source using Antennas for Propulsion,25th Int. Symposium on Space Technology and Science ISTS 2006-b-31,2006.06.
44. N. Sakaguchi, Y. Kajimura, H. Nakashima,Thrust Efficiency Calculation for Magnetic Nozzle in Laser Fusion Rocket,Trans. Jpn. Society for Aeronautical and Space Sciences, Vol.48, No.161, pp.180-182(2005),2005.12.
45. Y. P. Zakharov, V. M. Antonov, E. L. Boyarinstev, A. V. Melekhov, V. G. Posukh, I. F. Shaikhislamov, H. Nakashima, K. V. Vchivkov,Influence of Non-MHD Flutes on the Efficiency of Energy Transfer from the Laser-Produced, ICF, and Space Exploding Plasmas to Magnetic Fields,Trans. Fusion Science and Technology, Vol.47, No.1T, pp.187-190(2005),2005.10.
46. M. Tanisho, H. Kataharada, N. Yamamoto, H. Nakashima,A Miniaturized Ion Thruster and Neutralizer with Microwave Discharge,56th Int. Astronautical Congress, IAC-05-CIAC-05-C4.4.02 (2005),2005.09.
47. H. Nakashima, Y. Kajimura, Y. Kozaki, Y. Zakharov,A Laser Fusion Rocket based on Fast Ignition Concept,56th Int. Astronautical Congress, IAC-05-CIAC-05-C4.4.02 (2005),2005.09.
48. K. Izumi, H. Masui, H. Nakashima, K. Shinyasiki, N. Yamamoto,Electromagnetic Field Analysis for Microwave Discharge Ion Engine using Multi-monople Antenna System,56th Int. Astronautical Congress, IAC-05-CIAC-05-C4.4.02 (2005),2005.08.
49. Y. Takao, H. Kataharada, T. Miyamoto, H. Masui, N. Yamamoto, H. Nakashima,Performance Test of Micro Ion Thruster of Microwave Discharge Type,Advance in Applied Plasma Science, Vol.5, (2005),2005.05.
50. Y. Takao, H. Masui, T. Miyamoto, H. Kataharada, H. Ijiri, H. Nakashima,Development of Small-Scale Microwave Discharge Ion Thruster,Vacuum,Vol. 73, pp.449-454,2004.01.
51. T. Miyamoto, K. Mii, T. NIshijima, H. Ijiri, Y. Takao,Development of a New Microwave Discharge Type Ion Engine,Vacuum,Vol.73, pp.391-396,2004.01.
52. Y. Mori, H. Nakashima, F. W. Baity, R. H. Goulding, M. D. Carter, D. O. Sparks,High Density Hydrogen Helicon Plasma in a Nonuniform Magnetic Field,Plasma Sources Science & Technology,vol. 13, pp.424-435,2004.01.
53. K. V. Vchivkov, H. Nakashima, Y. P. Zakharov, T. Esaki, T. Kawano, T. Muranaka,Laser-Produced Plasma Experiments and Particle in Cell Simulation to Study Thrust Conversion Processes in a Laser Fusion Rocket,Jpn. J. Applied Physics　,Vol.42, No.10, pp.6590-6597,2003.10.
54. Y. Takao, T. Miyamoto, K. Yamawaki, T. Maeyama, H. Nakashima,Development of ECR Microwave Discharge Ion Thruster,Vacuum,Vol. 65, pp.361-366,2002.01.
55. T. Muranka, H. Uchimura, H. Nakashima, Y. Zakharov,Analysis on Exploding Plasma Behavior in a Dipole Magnetic Field,Jpn J. Applied Physics,Vol.40, pp824-831,2001.01.
56. H. Nakashima, Y. Nagamine, N. Yoshimi, Y. P. Zakharov,A. G. Ponomarenko,Use of Ignition Facility for Fusion Propulsion Experiment,J. Fusion Engineering and Design,Vol.44,pp.359-363,1999.01.
57. Y. Nagamine, H. Nakashima,Analysis of Plasma Behavior in a Magnetic Thrust Chamber of
Laser Fusion Rocket,Fusion Technology,Vol. 35, pp.62-70,1999.01.
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