Publication

Journal and conference papers by laboratory's members are listed below.
Please also visit JAXA's repository or CiNii database for further information.

2014

Academic journal

  1. Takahiro Nakamura, Hiroyuki Nishida, Shunjiro Shinohara, Ikkoh Funaki, Takao Tanikawa, Tohru Hada, Preliminary Investigation of Electromagnetic Thrust Characteristics in Electrodeless Compact Helicon Plasma Thruster, Transactions of the Japan Society for Aeronautical and Space Sciences, Aerospace Technology Japan, Vol. 12, No.ists29, pp.Po_1_1-Po_1_6, 2014. DOI:10.2322/tastj.12.Po_1_1
  2. Hiroki Watanabe, Masakatsu Nakano, Yoshihiro Kajimura, Ikkoh Funaki, Feasibility Study on Numerical Life Qualification of Ion Thruster's Ion Optics Using the JIEDI Tool, Transactions of the Japan Society for Aeronautical and Space Sciences, Aerospace Technology Japan, Vol. 12, No.ists29, pp.Pb_65-Pb_72, 2014. DOI:10.2322/tastj.12.Pb_65
  3. Shinohara, S. ; Nishida, H. ; Tanikawa, T. ; Hada, T. ; Funaki, I. ; Shamrai, K.P., Development of Electrodeless Plasma Thrusters With High-Density Helicon Plasma Sources, Plasma Science, IEEE Transactions on (Volume:42 , Issue: 5 )
  4. Yoshihiro KAJIMURA, Ikkoh FUNAKI, Iku SHINOHARA, Hideyuki USUI, Masaharu MATSUMOTO and Hiroshi YAMAKAWA, Numerical Simulation of Dipolar Magnetic Field Inflation due to Equatorial Ring-Current, Plasma and Fusion Research, Volume 9, 2405008 (2014)
  5. Yuya OSHIO, Kazuma UENO, Ikkoh FUNAKI, Hiroshi YAMAKAWA, Thrust Measurement of Magnetoplasma Sail in Laboratory Experiment, Transactions of the Japan Society for Aeronautical and Space Sciences, Aerospace Technology Japan,Vol. 12 (2014) No. ists29 p. Pb_45-Pb_51, DOI:http://dx.doi.org/10.2322/tastj.12.Pb_45
  6. Akira KAWASAKI, Kenichi KUBOTA, Ikkoh FUNAKI, Yoshihiro OKUNO, MHD Simulation and Thermal Design of an MPD Thruster, Trans. JSASS, Aerospace Technology Japan, Vol.12, No.ists29, 2014, p.Pb_19-Pb_25. DOI:10.2322/tastj.12.Pb_19
  7. Hikaru ARITA, Hiroyuki NISHIDA, Ikkoh FUNAKI, Magnetohydrodynamic Analysis of Thrust Characteristics on Magneto-Plasma Sail with Plasma Magnetic Field Inflation by Low-Beta Plasma, Trans. JSASS, Aerospace Technology Japan, Vol.12, No.ists29, 2014, p.Pb_39-Pb_44. DOI:10.2322/tastj.12.Pb_39
  8. Yasumasa ASHIDA, Ikkoh FUNAKI, Hiroshi YAMAKAWA, Yoshihiro KAJIMURA, Analysis of Small-scale Magneto Plasma Sail and Propulsive Characteristics, Trans. JSASS, Aerospace Technology Japan, Vol.12, No.ists29, 2014, p.Tb_11-Tb_18. DOI:10.2322/tastj.12.Tb_11
  9. Ashida, Y., Yamakawa, H., Funaki, I., Usui, H., Kajimura, Y., Kojima, H., Thrust evaluation of small-scale magnetic sail spacecraft by three-dimensional particle-in-cell simulation, Journal of Propulsion and Power, Vol.30, 2014, pp.186-196. DOI:10.2514/1.B35026
  10. Ashida, Y., Funaki, I., Yamakawa, H., Usui, H., Kajimura, Y., Kojima, H., Two-dimensional particle-in-cell simulation of magnetic sails, Journal of Propulsion and Power, Vol.30, 2014, pp.233-245. DOI:10.2514/1.B34692

Academic conferences

  1. T. Nakamura, S. Ito, H. Nishida, S. Shinohara, I. Funaki, T. Tanikawa, Thrust Performance of High Magnetic Field Permanent Magnet Type Helicon Plasma Thruster, AIAA-2014-3474, AIAA Propulsion and Energy, Cleveland, July 28-30, 2014.
  2. A. Kawasaki, K. Kubota, I. Funaki, Y. Okuno, Numerical Simulation of Plasma Flow in a Self-field MPD Thruster Coupled with Electrode Sheath, AIAA-2014-3696, AIAA Propulsion and Energy, Cleveland, July 28-30, 2014.
  3. K. Kubota, H. Watanabe, N. Yamamoto, H. Nakashima, T. Miyasaka, I. Funaki, Numerical Simulation of Microwave Neutralizer Including Ion’s Kinetic Effects, AIAA-2014-3831, AIAA Propulsion and Energy, Cleveland, July 28-30, 2014.
  4. S. Takagi, T. Morozumi, K. Matsuoka, J. Kasahara, A. Matsuo, I. Funaki, Study on Pulse Detonation Rocket Engine Using Flight Test Demonstrator "Todoroki II", AIAA-2014-4033, AIAA Propulsion and Energy, Cleveland, July 28-30, 2014.
  5. Y. Kato, K. Gawahara, K. Matsuoka, J. Kasahara, A. Matsuo, I. Funaki, Thrust Measurement of Rotating Detonation Engine by Sled Test, Oral Presentation, AIAA Propulsion and Energy, Cleveland, July 28-30, 2014.
  6. Y. Oshio, I. Funaki, K. Ueno, H. Yamakawa, Experimental Investigation of Magnetoplasma Sail with High Beta Plasma Jet, AIAA-2014-3959, AIAA Propulsion and Energy, Cleveland, July 28-30, 2014.
  7. I. Funaki, K. Kubota, A. Kawasaki, Y. Okuno, K. Miyazaki, S. Takenaka, H. Horisawa, Analysis of Self-field MPD Thrusters for Designing a Megawatt-class In-space Propulsion System, AIAA-2014-3418, AIAA Propulsion and Energy, Cleveland, July 28-30, 2014.
  8. A. Kawasaki, K. Kubota, I. Funaki, Y. Okuno, Numerical Study of Plasma Flow and Electrode Sheath in a Magnetoplasmadynamic Thruster, Asian Joint Conference on Propulsion and Power 2014, AJCPP-2014-20, Jeju, Korea, Mar.5-8, 2014.
  9. Y. Ashida, H. Yamakawa, I. Funaki, Y. Kajimura, Three-dimensional Full Kinetic Analysis on Propulsive Characteristics of Magneto Plasma Sail, Asian Joint Conference on Propulsion and Power 2014, AJCPP-2014-60, Jeju, Korea, Mar.5-8, 2014.
  10. I. Funaki, K. Kubota, K. Miyazaki, S. Takenaka, H.Horisawa, A. Kawasaki, Y. Okuno, Research and Development of High-power Self-field MPD Thruster, Asian Joint Conference on Propulsion and Power 2014, AJCPP-2014-136, Jeju, Korea, Mar.5-8, 2014.
  11. I. Funaki, Y. Kawakatsu, Future Low-cost Interplanetary Missions Following DESTINY, Asian Joint Conference on Propulsion and Power 2014, AJCPP-2014-137, Jeju, Korea, Mar.5-8, 2014.
  12. K. Ueno, M. Horie, Y. Oshio, I. Funaki, H. Yamakawa, An Experimental Study on the Forces of Magnetic Sails, Asian Joint Conference on Propulsion and Power 2014, AJCPP-2014-184, Jeju, Korea, Mar.5-8, 2014.
  13. T. Nakamura, S. Ito, H. Nishida, S. Shinohara, I. Funaki, T. Hada, T. Tanikawa, Development of High Magnetic Field Compact Helicon Plasma Thruster Utilizing Permanent Magnets, Asian Joint Conference on Propulsion and Power 2014, AJCPP-2014-134, Jeju, Korea, Mar.5-8, 2014.
  14. Tomohito Morozumi, Ryuki Sakamoto, Takashi Kashiwazaki, Jiro Kasahara, Ken Matsuoka, Akiko Matsuo, and Ikkoh Funaki, Study on a Rotary-Valved Four-Cylinder Pulse Detonation Rocket : Thrust Measurement by Ground Test, 52nd Aerospace Sciences Meeting, AIAA 2014-1317, Maryland, January 2014.
  15. Ken Matsuoka, Shunsuke Takagi, Jiro Kasahara, Tomohito Morozumi, Takashi Kashiwazaki, Yutaka Fujiwara, Akiko Matsuo, and Ikkoh Funaki, Study on a Rotary-Valved Four-Cylinder Pulse Detonation Rocket: Six Degree-of-Freedom Flight Measurement, 52nd Aerospace Sciences Meeting, AIAA 2014-1319, Maryland, January 2014.