Publication

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

2013

Academic journal

  1. Yoh Nagasaki, Taketsune Nakamura, Ikkoh Funaki, Yasumasa Ashida, and Hiroshi Yamakawa, Conceptual Design of YBCO Coil with Large magnetic Moment for Magnetic Sail Spacecraft, IEEE Transactions on Applied Superconductivity, Vol.23, No.3, 2013, 4603405, 4 pages.
  2. I. Funaki, Y. Kajimura, Y. Ashida, H. Nishida, Y. Oshio, I. Shinohara, H. Yamakawa, The Use of Dipole Plasma Equilibrium for Magnetic Sail Spacecraft, Transactions of Fusion Science and Technology,Vol.63, No.1T, 2013, pp.168-171.
  3. S. Shinohara, T. Tanikawa, T. Hada, I. Funaki, H. Nishida, T. Matsuoka, F. Otsuka, K. P. Shamrai, T. S. Rudenko, T. Nakamura, A. Mishio, H. Ishii, N. Teshigahara, H. Fujitsuka, S. Waseda, High-Density Helicon Plasma Sources: Basics And Application to Electrodeless Electric Propulsion, Fusion Science and Technology, Vol.63, No.1T, 2013, pp.164-167.
  4. K. Ueno, Y. Oshio, I. Funaki and H. Yamakawa., Experimental Simulation of Magnetoplasma Sail for Thrust Measurement, Fusion Science and Technology, Vol.63, No.1T, 2013, pp.392-394.
  5. Hisahiro Nakayama, Jiro Kasahara, Akiko Matsuo, and Ikkoh Funaki, Front Shock Behavior of Stable Curved Detonation Waves in Rectangular-Cross-Section Curved Channels, Proceedings of the Combustion Institute 34 (2013) pp.1939-1947, DOI:10.1016/j.proci.2012.06.012.
  6. Kazuma Ueno, Yuya Oshio, Ikkoh Funaki, Hideyuki Horisawa, and Hiroshi Yamakawa, Thrust Measurement of Magnetic Sail for Various Tilt Angles, Transactions of the Japan Society for Aeronautical and Space Sciences, Aerospace Technology Japan, Vol.10, 2012, pp.Tb_13-Tb_16, DOI:10.2322/tastj.10.Tb_13.
  7. Hisahiro Nakayama, Jiro Kasahara, Akiko Matsuo, and Ikkoh Funaki, Front Shock Behavior of Stable Curved Detonation Waves in Rectangular-Cross-Section Curved Channels, Proceedings of the Combustion Institute 34 (2013) pp.1939-1947, DOI:dx.doi.org/10.1016/j.proci.2012.06.012.
  8. Horisawa, H., Sumida, S., Yonamine, H., and Funaki, I., Thrust Generation through Low-Power Laser-Metal Interaction for Space Propulsion Applications, Vacuum, Vol.88, No.1, 2013, pp.75-78, DOI:10.1016/j.vacuum.2012.03.031 10.1016/j.vacuum.2012.03.031

Academic conferences

  1. N. Yamamoto, T. Miyasaka, K. Komurasaki, H. Koizumi, T. Schőnherr, H. Tahara, H. Takegahara, J. Aoyagi, M. Nakano, I. Funaki, H. Watanabe, Y. Ohkawa, A. Kakami, Y. Takao, S. Yokota, Developments of Robust Anode-layer Intelligent Thruster for Japan IN-space propulsion system, 33rd International Electric Propulsion Conference, IEPC-2013-244, Washington, Oct.6-10, 2013.
  2. S. Tonooka, I. Funaki, T. Matsuoka, S. Iwabuchi, T. Nakamura, S. Shinohara, H. Nishida, Thrust Characteristics of Helicon Plasma Thrusters, 33rd International Electric Propulsion Conference, IEPC-2013-253, Washington, Oct.6-10, 2013.
  3. K. Miyazaki, S. Takenaka, I. Funaki, and H. Horisawa, Experimental Study of a 1-MW-Class Quasi-Steady-State Self-Field Magnetoplasmadynamic Thruster, 33rd International Electric Propulsion Conference, IEPC-2013-234, Washington, Oct.6-10, 2013.
  4. K. Kubota, H. Watanabe, I. Funaki, N. Yamamoto, H. Nakashima, T. Miyasaka, Three-dimensional Hybrid-PIC Simulation of Microwave Neutralizer, 33rd International Electric Propulsion Conference, IEPC-2013-098, Washington, Oct.6-10, 2013.
  5. H. Watanabe, I. Funaki and R. Takaki, M. Nakano, Y. Kajimura, Sensitivity Analysis on Ion Acceleration Grid Erosion in Ion Thrusters, 33rd International Electric Propulsion Conference, IEPC-2013-268, Washington, Oct.6-10, 2013.
  6. A. Kawasaki, K. Kubota, I. Funaki, Y. Okuno, MHD and Thermal Simulations of a Radiation Cooled Self-field MPD Thruster, 33rd International Electric Propulsion Conference, IEPC-2013-262, Washington, Oct.6-10, 2013.
  7. Y. Oshio, Kazuma Ueno and Ikkoh Funaki, Hiroshi Yamakawa, Experimental Investigation of Thrust Characteristics of Magnetoplasma Sail, 33rd International Electric Propulsion Conference, IEPC-2013-160, Washington, Oct.6-10, 2013.
  8. Y. Ashida, I. Funaki, H. Yamakawa, Y. Kajimura, Full Kinetic Analysis of Small-scale Magneto Plasma Sail in Magnetized Solar Wind, 33rd International Electric Propulsion Conference, IEPC-2013-105, Washington, Oct.6-10, 2013.
  9. S. Shinohara, T. Tanikawa, T. Hada, I. Funaki, H. Nishida, F. Otsuka, D. Kuwahara, K. P. Shamrai, Characterization of High-density Helicon Plasma Sources and Application to Electrodeless Plasma Thrusters, 2013 Asia-Pacific Radio Science Conference (AP-RASC'13), HGa-4, Taipei, Taiwan, 2013.
  10. T. Hada, F. Otsuka, S. Shinohara, H. Nishida, T. Tanikawa, I. Funaki, Development of Electrodeless Helicon Plasma Thrusters, 2013 Asia-Pacific Radio Science Conference (AP-RASC'13), HGa-5 Taipei, Taiwan, 2013.
  11. H. Watanabe, M. Nakano, Y. Kajimura, I. Funaki, R. Takaki, Research and Development of Simulation Tool for Lifetime Evaluation of Ion Thruster in JAXA, 2013 Asia-Pacific Radio Science Conference (AP-RASC'13), HGb-1, Taipei, Taiwan, 2013.
  12. I. Funaki, H. Yamakawa, An Overview of Spacecraft Propulsion using the Solar Wind, 2013 Asia-Pacific Radio Science Conference (AP-RASC'13), HGb-2, Taipei, Taiwan, 2013.
  13. Y. Kajimura, I. Funaki, I. Shinohara, K. Ueno, Y. Oshio, H. Yamakawa, Numerical Simulation of Plasma Flow around a Magnetized Plasma Sail with a magnetic Nozzle, 2013 Asia-Pacific Radio Science Conference (AP-RASC'13), HGb-3, Taipei, Taiwan, 2013.
  14. T. Tanikawa, S. Shinohara, H. Nishida, T. Hada, F. Otsuka and I. Funaki, Plasma Acceleration via Externally Exerted Oscillating Electromagnetic Fields: Basic Physics and Application to Electrodeless Electric Propulsion, 12th Asia Pacific Physics Conference, APPC2012, D1-3-03, Chiba, July 14-19, 2013.
  15. Kiyoshi Kinefuchi, Koichi Okita, Ikkoh Funaki, Takashi Abe, Prediction of In-flight Radio Frequency Attenuation by a Rocket Plume by Applying CFD/FDTD Coupling, AIAA 2013-3790, 49th AIAA/ASME/SAE/ASEE Joint Propulsion Conference & Exhibit, San Jose, July 2013.
  16. Ikkoh Funaki, Yoshihiro Kajimura, Hiroyuki Nishida, Hiraku Arita, Yasumasa Ashida, Hiroshi Yamakawa, Yuya Oshio, Kazuma Ueno, Haruhito Yamamura, and Yoshiki Yamagiwa, Magnetoplasma Sail with Equatorial Ring-current, AIAA 2013-3878, 49th AIAA/ASME/SAE/ASEE Joint Propulsion Conference & Exhibit, San Jose, July 2013.
  17. Hiroki Watanabe, Masakatsu Nakano, Yoshihiro Kajimura, Ikkoh Funaki, and Ryoji Takaki, Numerical Life Qualification of Ion Thruster’s Ion Optics using the JIEDI Tool, AIAA 2013-3889, 49th AIAA/ASME/SAE/ASEE Joint Propulsion Conference & Exhibit, San Jose, July 2013.
  18. S. Shinohara, H. Nishida, T. Tanikawa, T. Hada, I. Funaki, K. P. Shamrai, Characterization of Developed High-Density Helicon Plasma Sources and Helicon Electrodeless Advanced Thruster (HEAT) Project, IEEE Pulsed Power & Plasma Science, PPPS2013, 6F-7, San Francisco, June16-21, 2013.
  19. T. Hada, F. Otsuka, S. Shinohara, H. Nishida, T. Tanikawa, and I. Funaki, Research and Development of Electrodeless Helicon Plasma Thrusters, 12th International Workshop on the Interrelationship between Plasma Experiments in the Laboratory and in Space, IPELS2013, I4-8, Hakuba, Japan, July 1-5, 2013.
  20. Takeshi Miyasaka, Kimiya Komurasaki, Hiroyuki Koizumi, Tony Schonherr, Naoji Yamamoto, Hirokazu Tahara, Haruki Takegahara, Masakatsu Nakano, Junichiro Aoyagi, Ikkoh Funaki, Hiroki Watanabe, Yasushi Okawa, Akira Kakami, Yoshiyuki Takao, Shigeru Yokota, Toshiyuki Ozaki, Hiroyuki Osuga, Overview on Developments of High-Power Hall Thruster with Anode Layer in Japan, 29th ISTS, 2013-o-1-01, Nagoya, June 2-9, 2013.
  21. Takahiro Nakamura, Hiroyuki Nishida, Shunjiro Shinohara, Ikkoh Funaki, Takao Tanikawa, Tohru Hada, Experimental Investigation of Thrust Characteristics in Lissajous Acceleration Type Electrodeless Helicon Plasma Thruster, 29th ISTS, 2013-o-1-08, Nagoya, June 2-9, 2013.
  22. Yuya Oshio, Kazuma Ueno, Ikkoh Funaki, Hiroshi Yamakawa, Thrust Measurement of Magnetoplasma Sail in Laboratory Experiment, 29th ISTS, 2013-b-05, Nagoya, June 2-9, 2013.
  23. Yoshihiro Kajimura, Ikkoh Funaki, Kazuma Ueno, Yuya Oshio, Hiroshi Yamakawa, Thrust Performance of a Magneto Plasma Sail with a Magnetic Nozzle, 29th ISTS, 2013-b-06, Nagoya, June 2-9, 2013.
  24. Shun Takenaka, Shun Takenaka, Naoto Yanagida, Naoto Kobayashi, Hideyuki Horisawa, Ikkoh Funaki, Characteristics of a Micro-Multi-plasmajet-Array Thruster, 29th ISTS, 2013-b-31, Nagoya, June 2-9, 2013.
  25. Kenichi Kubota, Hiroki Watanabe, Ikkoh Funaki, Naoji Yamamoto, Hideki Nakashima, Takeshi Miyasaka, Development of Hybrid-PIC Solver for Microwave Neutralizer, 29th ISTS, 2013-b-38, Nagoya, June 2-9, 2013.
  26. Yasumasa Ashida, Ikkoh Funaki, Hiroshi Yamakawa, Yoshihiro Kajimura, Numerical Analysis of Small-scale Magneto Plasma Sail and Propulsive Characteristics, 29th ISTS, 2013-b-42, Nagoya, June 2-9, 2013.
  27. Hiroki Watanabe, Hiroki Watanabe, Masakatsu Nakano, Yoshihiro Kajimura, Ikkoh Funaki, Feasibility Study on Numerical Life Qualification of Ion Thruster’s Ion Optics Using the JIEDI Tool, 29th ISTS, 2013-b-43, Nagoya, June 2-9, 2013.
  28. Kazuma Ueno, Yuya Oshio, Ikkoh Funaki, Hiroshi Yamakawa, Development of Magnetoplasmadynamic Solar Wind Simulator for Magnetoplasma Sail Experiment, 29th ISTS, 2013-b-46, Nagoya, June 2-9, 2013.
  29. Yasuhiro Kawakatsu, Kazutaka Nishiyama, Ikkoh Funaki, Takahiro Iwata, DESTINY Mission Description and Its Value, 29th ISTS, 2013-k-47, Nagoya, June 2-9, 2013.
  30. Hikaru Arita, Hiroyuki Nishida, Ikkoh Funaki, Magnetohydrodynamic Analysis of Thrust Characteristics on Magneto-Plasma Sail with Plasma Magnetic Field Inflation by Low-Beta Plasma, 29th ISTS, 2013-q-18, Nagoya, June 2-9, 2013.
  31. T. Hada, F. Otsuka, S. Shinohara, H. Nishida, T. Tanikawa, and I. Funaki, Electrodeless Plasma Thrusters: Nonlinear wave acceleration of a helicon plasma, 9th International Nonlinear Wave and Chaos Workshop, Mar.3-8, San Diego, LaJolla, 2013.
  32. Tomohito Morozumi, Ken Matsuoka, Ryuki Sakamoto, Ken Ikeguchi, Taiga Sakumi, Jiro Kasahara, Akiko Matsuo, Ikkoh Funaki, Sutdy on a Four-Cylinder Pulse Detonation Rocket Engine with a Coaxial High Frequency Rotary Valve, 51st Aerospace Sciences Meeting, Jan.7-10 2013.