Benjamin Jorns, Ioannis Mikellides, Stéphane Mazouffre, and Hiroyuki Koizumi, "Physics of electric propulsion," Journal of Applied Physics 132, 110401 (2022); https://doi.org/10.1063/5.0118076
Lev, D., Myers, R. M., Lemmer, K. M., Kolbeck, J., Koizumi, H., Polzin, k., "The technological and commercial expansion of electric propulsion," Acta Astronautica, Vol. 159 (2019), pp.213-227. Doi: 10.1016/j.actaastro.2019.03.058.
Levchenko, I., Bazaka, K., Ding, Y., Raitses, Y., Mazouffre, S., Henning, T., Klar, P. J., Shinohara, S., Schein, J., Garrigues, L., Kim, M., Lev, D., Taccogna, F., Boswell, R. W., Charles, C., Koizumi, H., Shen, Y., Scharlemann, C., Keidar, M., and Xu, S., "Space micropropulsion systems for Cubesats and small satellites: From proximate targets to furthermost frontiers," Applied Physics Reviews, Vol.5, No.1, p.011104 (2018). Doi:10.1063/1.5007734
小泉宏之: 超小型深宇宙探査機PROCYON 推進系：開発から宇宙運用までの道のりと教訓, プラズマ・核融合学会誌, Vol.92, No.7, pp. 501‐513, 2016.
イオンスラスタ関連
Hokuto Sekine, Ryo Minematsu, Yasuho Ataka, Pierre Ominetti, Hiroyuki Koizumi, and Kimiya Komurasaki, "Experimental characterization of non-Maxwellian electron energy distributions in a miniaturized microwave plasma neutralizer," Journal of Applied Physics, 131, 093302 (2022). doi: 10.1063/5.0069600
Yasuho Ataka, Yuichi Nakagawa, Hiroyuki Koizumi, Kimiya Komurasaki, "Improving the performance of a water ion thruster using biased electrodes," Acta Astronautica, Vol.187, pp.133-140 (2021). Doi: 10.1016/j.actaastro.2021.06.020
Nakano, M., Nakamura, K., Nakagawa, Y., Takao, Y., Koizumi, H., "Design of High Efficiency Grid System for Water Propellant Miniature Ion Thrusters," Transactions of Japan Soc. for Aeronautical and Space Sci., Aerospace Technology Japan, Vol. 18, No.6, pp.412-416 (2020). Doi: 10.2322/tastj.18.412
Y. Nakagawa, H. Koizumi, Y. Naito, and K. Komurasaki, “Water and xenonECR ion thruster—comparison in global model and experiment,” PlasmaSources Science and Technology, Vol.29, No.10 (2020). Doi: 10.1088/1361-6595/aba2ac
Sato, Y., Koizumi, H., Nakano, M., and Takao, Y., "Electron loss mechanisms in a miniature microwave discharge water neutralizer, " Physics of Plasmas 27, 063505 (2020). Doi: 10.1063/5.0002336
Sato, Y., Koizumi, H., Nakano, M., and Takao, Y., "Electron extraction enhancement via the magnetic field in a miniature microwave discharge neutralizer, " Journal of Applied Physics, Vol. 126, 243302 (2019). Doi: 10.1063/1.5127805
Nakamura, K., Koizumi, H., Nakano, M., and Takao, Y., "Effects of negative ions on discharge characteristics of water plasma source for a miniature microwave discharge ion thruster, " Physics of Plasmas, Vol. 26, 043508 (2019). Doi: 10.1063/1.5092754
Nakano, M., Nakamura, K., Naito, Y., Nakagawa, Y., Takao, Y., and Koizumi, H., "Computational design of a high-efficiency accelerator grid for a miniature ion thruster by full-aperture ion optics simulations," AIP Advances, Vol. 9, 035343 (2019). Doi: 10.1063/1.5090413
Nakagawa, Y., Koizumi, H., Kawahara, H., and Komurasaki, K., "Performance characterization of a miniature microwave discharge ion thruster operated with water," Acta Astronautica, Vol. 157, pp. 294-299, (2019). Doi:10.1016/j.actaastro.2018.12.031
Nakagawa, Y., Tomita, D., Koizumi, H., and Komurasaki, K., "Design and Test of a 100 μN-class Thrust Stand for a Miniature Water Ion Thruster with CubeSat," Transactions of Japan Soc. for Aeronautical and Space Sci., Aerospace Technology Japan, Vol.16 (2018), No.7, pp.673-678. DOI:10.2322/tastj.16.673
Nakamura, K., Nakagawa, Y., Koizumi, H., and Takao, Y., “Numerical Analysis of a Miniature Microwave-discharge Ion Thruster Using Water as the Propellant,” Transactions of Japan Soc. for Aeronautical and Space Sci., vol. 61, 2018, pp. 152–159, Doi: 10.2322/tjsass.61.152
Nakano, M., Nakamura, K., Nakagawa, Y., Tomita, D., Takao, Y., and Koizumi, H., "Numerical simulation of full-aperture-pair ion optics in a miniature ion thruster," Physics of Plasmas, Vol. 25, p. 013524 (2018). doi: 10.1063/1.5008802
Koizumi, H., Komurasaki, K., Aoyama, J., and Yamaguchi, K., "Development and Flight Operation of a Miniature Ion Propulsion System," Journal of Propulsion and Power, Vol. 34, No. 4 (2018), pp. 960-968. doi: 10.2514/1.B36459
Hiramoto, K., Nakagawa, Y., Koizumi, H., and Takao, Y., "Effects of E × B drift on electron transport across the magnetic field in a miniature microwave discharge neutralizer," Physics of Plasmas, Vol. 24, No. 6, Jun. 2017, p. 064504 (5pp). doi: 10.1063/1.4989734
Takao, Y., Hiramoto, K., Nakagawa, Y., Kasagi, Y., Koizumi, H., and Komurasaki, K., “Electron extraction mechanisms of a micro-ECR neutralizer,” Japanese Journal of Applied Physics, Volume 55, Number 7S2, 2016
Koizumi, H., Kawahara, H., Yaginuma, K., Asakawa, J., Nakagawa, Y., Nakamura, Y., Kojima, S., Matsuguma, T., Funase, R., Nakatsuka, J., and Komurasaki, K., Initial Flight Operations of the Miniature Propulsion System installed on Small Space Probe: PROCYON, Transactions of Japan Soc. for Aeronautical and Space Sci., Aerospace Technology Japan, Voll. 14, Pb_13-Pb_22, 2016.
Takao, Y., Koizumi, H., Kasagi, Y., and Komurasaki, K., “Investigation of Electron Extraction from a Microwave Discharge Neutralizer for a Miniature Ion Propulsion System,” Transactions of the Japan Society for Aeronautical and Space Sciences, Aerospace Technology Japan, Vol. 14, No. ists30, Sep. 2016, pp. Pb_41–Pb_46.
Takao, Y., Koizumi, H., Komurasaki, K., Eriguchi, K., and Ono, K., “Three-dimensional particle-in-cell simulation of a miniature plasma source for a microwave discharge ion thruster,“ Plasma Sources Sci. Technol., 23 064004, 2014.
Koizumi, H. Komurasaki, K., Aoyama, J., and Yamaguchi, K.,“Engineering Model of the Miniature Ion Propulsion System for the Nano-satellite,“Trans. JSASS Space Tech. Japan, Vol. 12, pp.Tb_19-Tb_24, 2014.
Sugita, Y., Koizumi, H., Kuninaka, H., Yamagiwa, Y., and Matsui, M., “Number Density Measurement of Neutral Particles in a Miniature Microwave Discharge Ion Thruster,” Trans. JSASS Space Tech. Japan, Vol. 12, pp.Tb_31-Tb_35, 2014.
Nakano, M., Koizumi, H., Inagaki, T., and Komurasaki, K., “Numerical Study of μ1 Ion Engine Optics Using JIEDI Tool,“Trans. JSASS Space Tech. Japan, Vol. 12, pp.Pb_27-Pb_32, 2014.
Tsukizaki, R., Ise, T., Koizumi, H., Togo, H., Nishiyama, K., and Kuninaka, H., “Thrust Enhancement of a Microwave Ion Thruster,” Journal of Propulsion and Power, Vol. 30, No. 5, pp.1383-1389, 2014.
Ise, T., Tsukizaki, R., Togo, H., Koizumi, H., and Kuninaka, H., "Electric field measurement in microwave discharge ion thruster with electro-optic probe," Rev. Sci. Instrum., Volume 83(2013), No.124702
Tsukizaki, R., Koizumi, H., Nishiyama, K., and Kuninaka, H., "Measurement of axial neutral density profiles in a microwave discharge ion thruster by laser absorption spectroscopy with optical fiber probes," Rev. Sci. Instrum. 82, 123103, 2011.
Koizumi, H. and Kuninaka, H., “Development of a Miniature microwave discharge ion thruster driven by 1 W microwave power,” Journal of Propulsion and Power, Vol26,No.3, pp.601-604, 2010.
Koizumi, H. and Kuninaka, H., “Switching Operation of Ion Beam Extraction and Electron Emission Using the Miniature Ion Thruster μ1,“Trans. JSASS Space Tech. Japan, Vol. 8, pp.Pb_85-Pb_90, 2010.
Tsukizaki, R., Koizumi, H., Hosoda, S., Nishiyama, K., and Kuninaka, H.,“Improvement of the Thrust Force of the ECR Ion Thruster μ10,“Trans. JSASS Space Tech. Japan, Vol. 8, pp.Pb_67-Pb_72, 2010.
Koizumi, H. and Kuninaka, H. “Antenna Design Method and Performance Improvement of a Micro Ion Engine Using Microwave Discharge," Trans. JSASS Space Tech. Japan, Vol. 7, pp.Pb_89-Pb_9, 2009
Hayashi, H., Nakayama, Y., Usui, M., Koizumi, H., Hosoda, S., Shimizu, Y., Nishiyama, K., and Kuninaka, H. "Experimental Demonstration of Microwave Discharge Ion Engine with 10,000 sec Isp," Trans. JSASS Space Tech. Japan, Vol. 7, pp.Tb_1-Tb_4, 2009
Koizumi, H. and Kuninaka, H., “Development and Characterization of a Low Power and Miniature Microwave Discharge Plasma Source”, Advances in Applied Plasma Science, Vol.7, pp.51–54, 2009.
K. Nishii, A. Hattori, H. Koizumi, K. Komurasaki, "Low-pressure-vaporization of water droplets on wall under normal and microgravity conditions," Acta Astronautica, Vol.186 (2021) pp.508-516. Doi: 10.1016/j.actaastro.2021.05.039
K. Nishii, H. Koizumi, and K. Komurasaki, "Experimental Characterization of Nozzle Performance at Low Reynolds Numbers for Water Microthrusters," Journal of Propulsion and Poower, 2021, DOI:10.2514/1.B38147
Kazuya YAGINUMA, Jun ASAKAWA, Yuichi NAKAGAWA, Yoshihiro TSURUDA, Hiroyuki KOIZUMI, Kota KAKIHARA, Kanta YANAGIDA, Yusuke MURATA, Mikihiro IKURA, Shuhei MATSUSHITA, Yoshihide AOYANAGI, Takeshi MATSUMOTO, "AQT-D: CubeSat Demonstration of a Water Propulsion System Deployed from ISS," Trans. JSASS Aerospace Technology Japan, 2020, Vol. 18, No. 4, pp.141-148,DOI:10.2322/tastj.18.141
K. Nishii, J. Asakawa, K. Kikuchi, M. Akiyama, Q. Wang, M. Murohara, Y. Ataka, H. Koizumi, R. Funase, K. Komurasaki, "Flight Model Development and Ground Demonstration of Water Resistojet Propulsion System for CubeSats," Trans. JSASS, 2020, Vol. 63, No. 4, pp.141-150,DOI:10.2322/tjsass.63.141
R. Funase, S. Ikari, K. Miyoshi, Y. Kawabata, S. Nakajima, S. Nomura, N. Funabiki, A. Ishikawa, K. Kakihara, S. Matsushita, R. Takahashi, K. Yanagida, D. Mori, Y. Murata, T. Shibukawa, R. Suzumoto, M. Fujiwara, K. Tomita, H. Aohama, K. Iiyama, S. Ishiwata, H. Kondo, W. Mikuriya, H. Seki, H. Koizumi, J. Asakawa, K. Nishii, A. Hattori, Y. Saito, K. Kikuchi, Y. Kobayashi, A. Tomiki, W. Torii, T. Ito, S. Campagnola, N. Ozaki, N. Baresi, I. Yoshikawa, K. Yoshioka, M. Kuwabara, R. Hikida, S. Arao, S. Abe, M. Yanagisawa, R. Fuse, Y. Masuda, H. Yano, T. Hirai, K. Arai, R. Jitsukawa, E. Ishioka, H. Nakano, T. Ikenaga, T. Hashimoto, "Mission to Earth–Moon Lagrange Point by a 6U CubeSat: EQUULEUS," in IEEE Aerospace and Electronic Systems Magazine, vol. 35, no. 3, pp. 30-44, 1 March 2020. Doi: 10.1109/MAES.2019.2955577
Asakawa, J., Nishii, K., Nakagawa, Y., Koizumi, H., and Komurasaki, K., "Direct measurement of 1-mN-class thrust and 100-s-class specific impulse for a CubeSat propulsion system, " Review of Scientific Instruments, Vol. 91, 035116 (2020). Doi: 10.1063/1.5121411
Koizumi, H., Asakawa, J., Nakagawa, Y., Nishii, K., Takao, Y., Nakano, M. and Funase, R., "Assessment of Micropropulsion System Unifying Water Ion Thrusters and Water Resistojet Thrusters," Journal of Spacecraft and Rocket, Vol. 56, No.5, 2019. Doi: 10.2514/1.A34407
Asakawa, J., Koizumi, H., Nishii, K., Takeda, N., Murohara, M., Funase, R., and Komurasaki, K., “Fundamental Ground Experiment of a Water Resistojet Propulsion System: AQUARIUS Installed on a 6U CubeSat: EQUULEUS,” Transactions of Japan Soc. for Aeronautical and Space Sci., Aerospace Technology Japan, Vol. 16, 2018, pp. 427–431. Doi: 10.2322/tastj.16.427
電磁誘導加速スラスタ関連
Sekine, H., Koizumi, H., and Komurasaki, K., "Measurement and identification of azimuthal current in an RF plasma thruster employing a time-varying magnetic field," AIP Advances 11, 015102 (2021).(Selected as Featured) doi: 10.1063/5.0029492
Sekine, H., Koizumi, H., and Komurasaki, K., "Electrostatic ion acceleration in an inductive radio-frequency plasma thruster," Physics of Plasmas 27, 103513 (2020). doi:10.1063/5.0020395
Kazuya Yaginuma, Hiroyuki Koizumi and Kimiya Komurasaki, Fundamental Experiment of Radio Frequency Inductive Plasma Accelerator with Low-Aspect Ratio RF-Plasma, プラズマ応用化学, Vol.23 No.2 (2015) pp.63-65
水／金属ハイブリッドスラスタ
Keita NISHII, Mariko AKIYAMA, Hiroyuki KOIZUMI, Kimiya KOMURASAKI, "Combustion of Magnesium Wires with Oxygen and Water Vapor," Combustion Science and Technology, pp.1-17 (2021). Doi: 10.1080/00102202.2021.2019241
Mariko AKIYAMA, Keita NISHII, Yoshihito MANNAMI, Masaya MUROHARA, Hiroyuki KOIZUMI, Kimiya KOMURASAKI, "Feasibility Study of a Hybrid Thruster using Wire-Shaped Magnesium and Water for Application to Small Spacecraft," Transactions of the Japan Society for Aeronautical and Space Sciences, Vol.64, Issue 4, pp.223-233 (2021). Doi: 10.2322/tjsass.64.223
水ホールスラスタ
K. Shirasu, H. Kuwabara, M. Matsuura, H. Koizumi, Y. Nakagawa, H. Watanabe, H. Sekine, and K. Komurasaki, "Demonstration and experimental characteristics of a water-vapor Hall thruster," J. Electric Propul., 2, 11 (2023). Doi: 10.1007/s44205-023-00047-w
小型固体スラスタ関連
Asakawa, J., Koizumi, H., Kojima, S., Nakano, M., and Komurasaki, K., "Laser-Ignited Micromotor Using Multiple Stacked Solid Propellant Pellets". Journal of Propulsion and Power, Vol. 35, No. 1 (2019), pp. 41-53. Doi:10.2514/1.B36715
Asakawa, J., Koizumi, H., Kojima, S., Nakano, M., Okada, N., and Komurasaki, K., "Total Impulse Increasing of a Micro-Solid Rocket Using a Stack of B/KNO3 Pellets", Transactions of Japan Soc. for Aeronautical and Space Sci., Aerospace Technology Japan, Vol. 14, Pa_53-Pa_59, 2016.
Hayashi, T., Koizumi, H., Asakawa, J., Nakano, M., and Komurasaki, K., "Ignition Probability Improvement of a Laser-Ignition Micro Solid Rocket," Trans. JSASS Space Tech. Japan, Vol. 12, pp.Tb_37-Tb_41, 2014.
Nakano, M., Koizumi, H. Watanabe, M., and Arakawa, Y., “Laser Ignition Microthruster Experiments on KKS-1," Trans. JSASS Space Tech. Japan, Vol. 8, pp.Pb_7-Pb_11, 2010
Nakano, M., Koizumi, H., Watanabe, M., and Arakawa, Y. "A Laser Ignition Microthruster for Microspacecraft Propulsion," Trans. JSASS Space Tech. Japan, Vol. 7, pp.Pb_7-Pb_9, 2009.
Koizumi, H., Inoue, T., Komurasaki, K., and Arakawa, Y., "Fundamental Characteristics of Laser Ablation Microthruster," Transactions of the Japan Society for Aeronautical and Space Sciences, Vol.50, No.167, pp.70-76, 2007.
Koizumi, H., Nakano, M., Inoue, T., Watanabe, M., Komurasaki, K., and Arakawa, Y., "Study on Laser Ignition of Boron / Potassium Nitrate in Vacuum," Science and Technology of Energetic Materials, Vo.67, No.6, pp.193-198, 2006.
Koizumi, H., Inoue, K., Nakano, M., and Arakawa, Y., "Dual Propulsive Mode Microthruster Using a Diode Laser," Journal of Propulsion and Power, Vol. 21, No. 6，pp.1133-1136，2005．
Ling, W., Schönherr, T., and Koizumi, H., "Discharge characteristics of an ablative pulsed plasma thruster with non-volatile liquid propellant," Applied Physics Letters, 111, 014101, 2017; doi: 10.1063/1.4991713.
Ling, W., Schönherr, T., and Koizumi, H., "Characteristics of a non-volatile liquid propellant in liquid-fed ablative pulsed plasma thrusters," Journal of Applied Physics 121, 073301, 2017; doi: 10.1063/1.4975349.
Schönherr, T., Cho, S.,Koizumi, H., Komurasaki, K., Yamamoto, N., Miyasaka, T., Kuninaka, H., "Japan's Itinerary Towards High-Power Electric Propulsion," Proceedings of the MAI, 60, 2012.
Kawara, S., Hamajima, E., Koizumi, H., Kousaka, H., Yamada, K., Umehara, N., and Arakawa, Y., "Investigation of Affecting Factors on the Hardness of Fluorine-Containing Amorphous Carbon Film Coated by Pulsed-Plasma Ablation," IEEE Transactions on Plasma Science Vol. 40 (2012), No. 7, pp.1820-1828.
Saito, T., Koizumi, H., and Kuninaka, H. "Pulsed Plasma Acceleration Using Powdered Propellant," J. Plasma Fusion Res. SERIES, Vol. 8, pp.1611-1615, 2009.
Koizumi, H., Noji, R., M., Komurasaki, K., and Arakawa, Y., "Plasma acceleration processes in an ablative pulsed plasma thruster," Physics of Plasmas, Vo.14, No.3, Article No.033506, 2007.
Koizumi, H., Kawazoe, Y., Komurasaki, K., and Arakawa, Y., "Effect of Solute Mixing in the Liquid Propellant of a Pulsed Plasma Thruster," Vacuum, Vol. 80, pp.1234-1238, 2006.
Koizumi, H., Kawazoe, Y., Komurasaki, K., and Arakawa, Y., "Effect of Seed on the Liquid Propellant of Pulsed Plasma Thruster," Advances in Applied Plasma Science, Vol. 5, pp. 157-162, 2005.
Koizumi, H., Komurasaki, K., and Arakawa, Y., "Development of Thrust Stand for Low Impulse Measurement from Microthrusters," Review of Scientific Instruments, Vol. 75, No. 10, pp.3185-3189, 2004.
Kakami, A., Koizumi, H., Komurasaki, K., and Arakawa, Y., "Design and performance of liquid propellant pulsed plasma thruster," Vacuum, Vol. 73, pp.419-425, 2004.
Kakami, A., Koizumi, H., Komurasaki, K., and Arakawa, Y., "Design and Performance of a Pulsed Plasma Thruster with Liquid Propellant," Advances in Applied Plasma Science, Vol. 4, pp. 127-132, 2003.
Y. Hamada, R. Kawashima, J. Bak, K. Komurasaki, and H. Koizumi, "Characterization of Acceleration Zone Shifting in an Anode-Layer-Type Hall Thruster RAIJIN66," Vacuum, 186:110040, 2021. Doi: 10.1016/j.vacuum.2020.110040
G. Ito, R. Kawashima, K. Komurasaki, and H. Koizumi, "Incident angle dependence of reflected particles in low-energy xenon-ion impacts on metal surfaces," Computational Materials Science, 186:109989, 2020. Doi: 10.1016/j.commatsci.2020.109989
Tabata, K., Harada, Y., Nakamura, Y., Komurasaki, K., Koizumi, H., Kariya, T., and Minami, R., "Experimental investigation of ionization front propagating in a 28 GHz gyrotron beam: Observation of plasma structure and spectroscopic measurement of gas temperature," Journal of Applied Physics, Vol. 127, 063301 (2020). Doi: 10.1063/1.5144157
Bak, J., Kawashima, R., Komurasaki, K., and Koizumi, H., "Plasma formation and cross-field electron transport induced by azimuthal neutral inhomogeneity in an anode layer Hall thruster," Physics of Plasmas, 26(7):073505, 2019. Doi:10.1063/1.5090931
Tanaka, S., Yamada, S., Soga, R., Komurasaki, K., Kawashima, R., and Koizumi, H., "Alumina reduction by laser ablation using a continuous-wave CO2 laser toward lunar resource utilization," Vacuum, 167:495-499, 2019. Doi:10.1016/j.vacuum.2018.07.054
Ito, G., Kawashima, R., Komurasaki, K., and Koizumi, H., "Inflow angular dependence of the capture coefficient in cryopumps," Vacuum, 160:102-108, 2019. Doi:10.1016/j.vacuum.2018.11.013. Doi:10.1016/j.vacuum.2018.11.013
Nakamura, Y., Komurasaki, K., Fukunari, M., and Koizumi, H., "Numerical analysis of plasma structure observed in atmospheric millimeter-wave discharge at under-critical intensity," Journal of Applied Physics 124, 033303 (2018), Doi: 10.1063/1.5023269
Hamada, Y., Bak, J., Kawashima, R., Koizumi, K., Komurasaki, K., Yamamoto, N., Egawa, Y., Funaki, I., Iihara, S., Cho, S., Kubota, K., Watanabe, H., Fuchigami, K., Tashiro, Y., Takahata, Y., Kakuma, T., Furukubo, Y., Tahara, H., "Hall Thruster Development for Japanese Space Propulsion Programs," Transactions of JSASS, 60(5):320-326, 2017.
Shimano, T., Ofosu, J. A., Matsui, K., Komurasaki, K., and Koizumi, H., "Laser-Induced Discharge Propagation Velocity in Helium and Argon Gases," Transactions of JSASS, 60(6):378-381, 2017. Doi:10.2322/tjsass.60.378
Matsui, K., Shimano, T., Ofosu, J. A., Komurasaki, K., Schoenherr, T., and Koizumi, H., "Accurate propagation velocity measurement of laser supported detonation waves," Wireless Engineering and Technology, Vacuum, v 136, p 171-176, 2017. Doi: 10.1016/j.vacuum.2016.07.011
Fukunari, M., Wongsuryrat, N., Yamaguchi, T., Nakamura, Y., Komurasaki, K., and Koizumi, H., "Design of a Millimeter-Wave Concentrator for Beam Reception in High-Power Wireless Power Transfer," WJournal of Infrared, Millimeter, and Terahertz Waves, Vol.38(2), pp.176-190, 2017. Doi: 10.1007/s10762-016-0327-0
Nako, S., Okuda, K., Miyashiro, K., Komurasaki, K., and Koizumi, H., "Wireless Power Transfer to a Microaerial Vehicle With a Microwave Active Phased Array," International Journal of Antennas and Propagation, p.374543, 2014. Doi: 10.1155/2014/374543
Shimamura, K., Ofosu, J.A., Komurasaki, K., and Koizumi, H., "Predicting propagation limits of laser-supported detonation by Hugoniot analysis," Japanese Journal of Applied Physics, Vol.54(1), p.016201, 2015. Doi: 10.7567/JJAP.54.016201
Shimamura, K., Komurasaki, K., Ofosu, J.A., Koizumi, H., "Precursor ionization and propagation velocity of a laser-absorption wave in 1.053 and 10.6-μm wavelengths laser radiation," IEEE Transactions on Plasma Science,Vol.42(10), pp.3121-3128, 2014. Doi: 10.1109/TPS.2014.2304960
Yamakawa, M., Shimamura, K., Komurasaki, K., and Koizumi, H., "Demonstration of Automatic Impedance-Matching and Constant Power Feeding to and Electric Helicopter via Magnetic Resonance Coupling," Wireless Engineering and Technology, 5(3):45-53, 2014.
Yamakawa, M., Mizuno, Y., Ishida, J., Komurasaki, K., and Koizumi, H., "Wireless Power Transmission into a Space Enclosed by Metal Walls Using Magnetic Resonance Coupling," Wireless Engineering and Technology, 5(1):19-24, 2014.
Ito, Y., Nakano, M., Schönherr, T., Cho, S., Komurasaki, K., and Koizumi, H., "Cost Evaluation of In-Space Transportation of a Solar Power Satellite Using OTVs with Hall Thruster Propulsion Systems," Transactions of Japan Soc. for Aeronautical and Space Sci., Aerospace Technology Japan, 12(ists29):Po_1_7-Po_1_12, 2014.
Fujita, D., Kawashima, R., Ito, Y., Akagi, S., Suzuki, J., Schönherr, T., Koizumi, H., and Komurasaki, K., "Operating Parameters and Oscillation Characteristics of an Anode-Layer Hall Thruster with Argon Propellant," Vacuum, 110:159-164, 2014.
Kawamura, S., Ando, M., Seto, N., et al., "The Japanese space gravitational wave antenna: DECIGO," CLASSICAL AND QUANTUM GRAVITY, Vol.28, No.9, 2011.
Koizumi, H. Komurasaki, K., and Arakawa, Y., "Numerical Prediction of Wall Erosion on a Hall Thruster," Vacuum, Vol. 83, pp.67-71, 2009.
Koizumi, H., Komurasaki, K., and Arakawa, Y., "Numerical Modeling of Wall Erosion on Hall Thrusters," Advances in Applied Plasma Science, Vol. 6, pp. 77-80, 2007.
Small Satellite Conference 2019, Student Poster Award, Second Place Keita NISHII "Pre-flight Testing of AQUARIUS: the Water Resistojet Thruster on the SLS EM-1 CubeSat for Deep Space Exploration" 2019 August 8, Logan, Utah, USA https://smallsat.org
The 32nd ISTS Japanese Rocket Society Award Yasuho ATAKA "Performance Evaluation of a 100 µN-Class Water Ion Thruster using Neodymium Magnets" 2018 June 22, Aossa and Happring, Fukui, Japan https://www.ists.or.jp/
IEPC2015 Best Paper Award by the Electric Rocket Propulsion Society Hiroyuki Koizumi, Hiroki Kawahara, Kazuya Yaginuma, Jun Asakawa, Ryu Funase, and Kimiya Komurasaki 「In-Flight Operation of the Miniature Propulsion System Installed on Small Space Probe: PROCYON」 2017 October 11, Atlanta, USA http://erps.spacegrant.org/index.php?page=best-paper
"Next Generation CubeSats and SmallSats - Enabling Technologies, Missions, and Markets," ELSEVIER Editors: Francesco Branz, Chantal Cappelletti, Antonio J. Ricco, John Hines, 2023 Paperback ISBN: 9780128245415, eBook ISBN: 9780128245422 August 24, 2023 Next Generation of CubeSats and SmallSats: Enabling Technologies, Missions, and Markets provides a comprehensive understanding of the small and medium sized satellite approach and its potentialities and limitations. The book analyzes promising applications (e.g., constellations and distributed systems, small science platforms that overachieve relative to their development time and cost) as paradigm-shifting solutions for space exploitation, with an analysis of market statistics and trends and a prediction of where the technologies, and consequently, the field is heading in the next decade. The book also provides a thorough analysis of CubeSat potentialities and applications, and addresses unique technical approaches and systems strategies.
Throughout key sections (introduction and background, technology details, systems, applications, and future prospects), the book provides basic design tools scaled to the small satellite problem, assesses the technological state-of-the-art, and describes the most recent advancements with a look to the near future. This new book is for aerospace engineering professionals, advanced students, and designers seeking a broad view of the CubeSat world with a brief historical background, strategies, applications, mission scenarios, new challenges and upcoming advances.
Chapter 19: "Dual-mode propulsion systems for SmallSats" by Joshua L. Rovey and Hiroyuki Koizumi
"The Nanosatellite Revolution: 30 Years and Continuing," SPIE Editors: Henry Helvajian; Siegfried W. Janson，2023 June 23, 2023 DOI: 10.1117/3.2618157 PDF ISBN: 9781510649347, Print ISBN: 9781510649330 This work assembles chapters from contributors across our planet to document technologies, applications, missions, licensing requirements, and lessons learned by individuals and organizations that have participated in the nanosatellite revolution. This book is not intended as a "how to" or as a university reference to design, build, and fly nanosatellites but as a deeper-level reference on what has and hasn't worked in previous nanosatellite programs. Many chapters act as a historical reference for particular programs.
Chapter 3: "One Year On-Orbit Operation of a Micropropulsion System Using an Ion Thruster and Cold-Gas Thrusters on the 50-Kg-Class Micro Space Probe, PROCYON" by Hiroyuki Koizumi
Deep Space Exploration and Micropropulsion Lecture series for the 7th Mission Idea Contest for Deep Space Science and Exploration with micro/nano satellites 2021年2月25日 http://www.spacemic.net/lecture.html
