雑誌論文

[29] S. Harada, T. Baba, A. Uchigashima, S. Yokota, A. Iwakawa, A. Sasoh, T. Yamazaki, H. Shimizu, “Electrostatic Acceleration of Helicon Plasma using a Cusped Magnetic Field,” Applied Physics Letters, 105, 194101 (2014).
[28] H. Tsuruta, B. Wang, Z. Wang, S. Yokota, and A. Sasoh “Repetitive Pulse Performance of One-Micrometer Laser-Ablation Propulsion onto Aluminum,” Jounal of Propulsion and Power, Vol. 30, No. 6, pp. 1485-1489.
[27] 市原大輔,原田翔太,片岡久志,横田茂,佐宗章弘,矩形断面形状を有する定常・外部磁場印加MPDスラスターの作動特性,日本航空宇宙学会誌論文集(in press).
[26] T. Osuka, E. Erdem, N. Hasegawa, R. Majima, T. Tamba, S. Yokota, A. Sasoh and K. Kontis, Laser energy deposition effectiveness on shock-wave boundary-layer interactions over cylinder-flare combinations, Phys. Fluids, 26, 096103 (2014).
[25] S. Cho, S. Yokota, K. Komurasaki, and Y. Arakawa, Multilayer Coating Method for Investigating Channel-Wall Erosion in a Hall Thruster, Journal of Propulsion and Power, Vol. 29(1), pp. 278-281, 2013.
[24] S. Yokota, D. Takahashi, S. Cho, R. Kaneko, M. Hosoda, K. Komurasaki, and Y. Arakawa, Magnetic Topology to Stabilize Ionization Oscillation in Anode-layer-type Hall Thruster, Transactions of the Japan Society for Aeronautical and Space Sciences, Aerospace Technology Japan, Vol.10, No.ists28, pp. Pb_31-Pb_35, 2012.
[23] S. Cho, S. Yokota, R. Kaneko, K. Komurasaki, and Y. Arakawa, Channel Wall Erosion Modeling of a SPT-Type Hall Thruster, Transactions of the Japan Society for Aeronautical and Space Sciences, Aerospace Technology Japan , Vol. 10, No.ists28, pp. Pb_25-Pb_30, 2012.
[22] D. Takahashi, S. Yokota, S. Cho, R. Kaneko, M. Hosoda, K. Komurasaki, and Y. Arakawa, Effect of Magnetic Field Configuration on Thrust Performance in Anode Layer Type Hall Thruster, Frontier of Applied Plasma Technology, Vol.4 (1), pp. 16-19, 2011.
[21] J. Yang, S. Yokota, R. Kaneko, and K. Komurasaki, Diagnosing on Plasma Plume from Xenon Hall Thruster with Collision-Radiative Model, Physics of Plasmas, Vol.17, 103504 (8 pages), 2010.
[20] S. Cho, S. Yokota, K. Hara, D. Takahashi, Y. Arakawa, K. Komurasaki, and A. Kobayashi, Development of Lifetime Evaluation Method Using Multilayer Coated Chip, Transactions of the Japan Society for Aeronautical and Space Sciences, Aerospace Technology Japan, Vol.8, No.ists26, pp. Pb_51-54, 2010.
[19] 金子亮太郎,横田茂,張科寅,原健太郎,高橋大祐,小紫公也,荒川義博,発光分光法によるホール型推進機の壁面損耗率評価,プラズマ応用科学,18巻1号,pp. 37-42,2010.
[18] 福島靖博,横田茂,小紫公也,荒川義博,周方向に非一様な周方向に非一様な推進剤供給によるアノードレイヤ型ホールスラスタの放電安定化,日本航空宇宙学会誌論文集,58巻672号,pp. 8-14, 2010.
[17] S. Yokota, M. Lempke, M. Matsui, K. Hara, K. Komurasaki and Y. Arakawa, Diagnostics of Xe Ion in an Anode-layer Type Hall Thruster Using Laser-Induced Fluorescence, Transactions of the Japan Society for Aeronautical and Space Science, Space Technology Japan, Vol. 7, No.ists26, pp. Pb_131-Pb_134, 2009.
[16] Y. Fukushima, S. Yokota, K. Komurasaki and Y. Arakawa, Influence of Azimuthally Nonuniform Propellant Flow Rate on Thrust Vector and Discharge Current Oscillation in a Hall Thruster, Transactions of the Japan Society for Aeronautical and Space Science, Space Technology Japan, Vol. 7, No.ists26, pp. Pb_41-Pb_45, 2009.
[15] S. Cho, S. Yokota, Y. Fukushima, K. Hara, Y. Arakawa, K. Komurasaki, and A. Kobayashi, Application of Lifetime Evaluation Method Using Multilayer Coated Chips, Plasma Application & Hybrid Functionally Materials, Vol. 18, p. 84, 2009.
[14] 張科寅, 横田茂,原健太郎,高橋大祐,荒川義博,小紫公也,小林明,多層コーティング損耗速度計測法の評価,プラズマ応用科学,17巻2号,pp. 154-158,2009.
[13] 張科寅, 横田茂,福島靖博,原健太郎,荒川義博,小紫公也,小林明,多層コーティングチップによる損耗速度計測,プラズマ応用科学,17巻1号,pp. 63-66,2009.
[12] S. Yokota, Y. Fukushima, R. Tsukizaki, K.Komurasaki, Y. Arakawa, A. Kobayashi, "Development of Hall Thruster Life Time Measurement Method Using Multilayer Coating Chip,” Frontier of Applied Plasma Technology, Vol. 1, pp.83-84, 2008.
[11] M. Lempke, S. Yokota, M. Matsui, K. Hara, K. Komurasaki, Y. Arakawa, “LIF Spectroscopy of a Hall Thruster Plasma Plume,” Frontier of Applied Plasma Technology, Vol. 1, pp.37-40, 2008.
[10] Yokota S., Sakoh D., Matsui M., Komuraski K., Arakawa Y., “Charge Exchange Ion Number Density Distribution in Hall Thruster Plume,” Vacuum, Vol. 83, pp.57-60, 2008.
[9] Nagao N., Yokota S., Komurasaki K., Arakawa Y., “ Development of a Two-dimensional Dual Pendulum Thrust Stand for Hall Thrusters,” Review of Scientific Instruments, Vol. 7, 115108, 2007.
[8] Sakoh D., Yokota S., Komurasaki K., Arakawa Y., “Charge Exchange Ions in a Hall Thruster Plume,” Advenced Applied Plasma Science, Vol. 6, pp. 65-68, 2007.
[7] Fukushima, Y., Yokota, S., Komurasaki, K., Arakawa, Y., Kobayashi, A., “Evaluation Method of Hall Thruster’s Lifetime by Using Multilayer Coating,” Transaction of JWRI, Vol. 36, No.1, 2007.
[6] 横田茂, 福島靖博, 佐孝大地, 小紫公也, 荒川義博, "多層コーティングによるホール型推進機の寿命評価法," プラズマ応用科学, Vol.15-1, pp. 61-64, Jun., 2007.
[5] 横田茂, 松井信, 佐孝大地, 小紫公也, 荒川義博, "ホール型推進機プルーム中のXe原子数密度測定," プラズマ応用科学, Vol.14, pp. 35-40, Dec., 2006.
[4] Yokota, S., Komurasaki, K., Arakawa, Y., "The Fluctuation of Electron Density Distribution Inside a Hollow Anode in an Anode-Layer Hall Thruster," Proceedings of the twenty fifth International Symposium on Space Technology and Science, (selected papers), 2006.
[3] 横田茂, 安井伸輔, 熊倉賢, 小紫公也, 荒川義博, "アノードレイヤ型ホールスラスタ内部のシース構造と放電電流の数値解析," 日本航空宇宙学会誌, Vol.54, No. 632, Sep., 2006.
[2] N., Yamamoto, S., Yokota, M., Matsui, K., Komurasaki, and Y., Arakawa, "Measurement of Erosion Rate by Absorption Spectroscopy in a Hall Thruster," Review of Scientific Instruments, American Institute of Physics, Vol. 76, No. 8, 083111., 2005.
[1] N., Yamamoto, S., Yokota, K., Watanabe, A., Sasoh, K., Komurasaki, Y., Arakawa, "A Suppression Method of Discharge Current Oscillations in a Hall Thruster," Trans. of Japanese Soc. for Aeronautical and Space Sci., The Japan Society For Aeronautical and Space Sciences, Vol.48, No.161, pp. 169- 174, 2005.

 

 

国際会議論文

[46] S. Yokota, D. Ichihara, H. Kataoka, S. Harada, and A. Sasoh, Steady-State, Applied-Field, Rectangular MPD Thrusters, 33rd International Electric Propulsion Conference, IEPC-2013-246, Online-server (8 pages), The George Washington University, October, 2013.
[45] N. Yamamoto, S. Yokota (15th author), et. al. Development of Robust Anode-Layer Intelligent Thruster for Japan IN-space Propulsion System, 33rd International Electric Propulsion Conference, IEPC-2013-244, Online-server (10 pages), The George Washington University, October, 2013.
[44] D. Ichihara, S. Harada, S. Yokota, and A. Sasoh, Steady-state, Magnetoplasmadynamic Thruster with Permanent Magnets, ISTS-2013-o-1-06, USB-flash-drive (7 pages), 29th International Symposium on Space Technology and Science, Nagoya, July, 2013.
[43] N. Hasegawa, S. Yokota, and A. Sasoh, Single-Plate-Imaging, Two-Wavelength, Mach-Zehnder Interferometer, 29th International Symposium on Shock Waves, 0246-000105, CD-ROM (6 pages), Madison, July, 2013.
[42] A. Sasoh, S. Harada, H. Tsuruta, and S. Yokota, Impulse Performance of Ablation Laser Propulsion with Repetitive 1-um Laser Pulses, Asian Joint Conference on Propulsion and Power 2012, AJCPP2012-023, CD-ROM (3 pages), Xian, March, 2012.
[41] A. Sasoh, D. Ichihara, T. Enoki, and S. Yokota, Development of Steady-State, Applied-field, Rectangular Magneto-Plasma-Dynamics (MPD) Thruster Using a Hollow Cathode, Asian Joint Conference on Propulsion and Power 2012, AJCPP2012-024, CD-ROM (3 pages), Xian, March, 2012.
[40] S. Yokota, M. Yonemoto, and A. Sasoh, Two-Dimensional, Applied-Field MPD Thruster Using a Hollow Cathode, 32nd International Electric Propulsion Conference, IEPC-2011-275, USB-flash-drive (7 pages), Wiesbaden, September, 2011.
[39] S. Cho, R. Kaneko, Y. Arakawa, K. Komurasaki, and S. Yokota, Experimental and Numerical Study on a Hall Thruster Insulator Erosion, 32nd International Electric Propulsion Conference, IEPC-2011-078, USB-flash-drive (9 pages), Wiesbaden, September, 2011.
[38] S. Yokota, D. Takahashi, S. Cho, R. Kaneko, M. Hosoda, K. Komurasaki, and Y. Arakawa, Ionization Oscillation Stabilization Method for Anode-Layer-Type Hall Thruster, 28th International Symposium on Space Technology and Science, ISTS-2011-b-25, USB-flash-drive (5 pages), Okinawa, June, 2011.
[37] S. Cho, S. Yokota, D. Takahashi, R. Kaneko, Y. Arakawa, and K. Komurasaki, Channel Wall Erosion Modeling of a SPT-type Hall Thruster, ISTS-2011-b-21, USB-flash-drive (4 pages), 28th International Symposium on Space Technology and Science, Okinawa, June, 2011.
[36] S. Cho, S. Yokota, Y. Arakawa, and K. Komurasaki, Development of Cylindrical Hall Thruster, 61st International Astronautical Congress, IAC-10.C4.4.5, CD-ROM (5 pages), Prague, September, 2010.
[35] S. Cho, S. Yokota, K. Hara, D. Takahashi, Y. Arakawa, K. Komurasaki, and A. Kobayashi, Hall Thruster Channel Wall Erosion Rate Measurement Method Using Multilayer Coated Chip, AIAA-2010-6697, CD-ROM (10 pages), 46th AIAA/ASME/SAE/ASEE Joint Propulsion Conference and Exhibit , Nashville, July, 2010.
[34] S. Yokota, R. Kaneko, S. Cho, K. Hara, D. Takahashi, K. Komurasaki, and Y. Arakawa, Erosion Measurement of a Hall Thruster Using Optical Emission Spectroscopy, AJCPP2010-122, CD-ROM (4 pages), Asian Joint Conference on Propulsion and Power 2010, Miyazaki, March, 2010.
[33] S. Cho, S. Yokota, K. Hara, D. Takahashi, Y. Arakawa, K. Komurasaki, and A. Kobayashi, Improvement of Erosion Rate Measurement Using Multilayer Coated Chip, Asian Joint Conference on Propulsion and Power 2010, AJCPP2010-085, CD-ROM (5 pages), Miyazaki, March, 2010.
[32] S. Cho, S. Yokota, K. Hara, D. Takahashi, Y. Arakawa, K. Komurasaki, and A. Kobayashi, Hall Thruster Channel Wall Erosion Rate Characteristics Measurement by Multilayer Coating Chip, The 17th Annual Meeting of IAPS, Proceedings of the 17th Annual Meeting of IAPS International Workshop, p.74, Busan, March, 2010.
[31] S. Yokota, R. Kaneko, S. Cho, K. Hara, D. Takahashi, K. Komurasaki, and Y. Arakawa, "Evaluation Method of Wall Erosion in Hall Thruster Using Optical Emission Spectroscopy," The 17th Annual Meeting of IAPS, Proceedings of the 17th Annual Meeting of IAPS International Workshop, pp.25-26, Busan, March, 2010.
[30] S. Yokota, K. Hara, S. Cho, D. Takahashi, K. Komurasaki, and Y. Arakawa, "Measurement of Ion Number Density and Velocity Distribution in an Anode-Layer Type Hall Thruster by Laser Induced Florescence Method," 31st International Electric Propulsion Conference, IEPC-2009-149, USB-flash-drive (7 pages), Ann Arbor, September, 2009.
[29] S. Yokota, Y. Fukushima, D. Takahashi, K. Hara, S. Cho, K. Komurasaki, and Y. Arakawa, Discharge Stabilization Method of an Anode Layer Type Hall Thruster by Non-uniform Propellant Flow, 31st International Electric Propulsion Conference, IEPC-2009-148, USB-flash-disk (8 pages), Ann Arbor, September, 2009.
[28] T. Schonherr, M. Lau, G. Herdrich, H. Roser, K. Komurasaki, S. Yokota, and Y. Arakawa, Cooperation Activities between IRS and the University of Tokyo in the Field of Pulsed Plasma Thruster Development, 31st International Electric Propulsion Conference, IEPC-2009-251, USB-flash-disk (6 pages) , Ann Arbor, September, 2009.
[27] S. Yokota, K. Hara, S. Cho, D. Takahashi, K. Komurasaki, and Y. Arakawa, The Difference between Anode Shapes in an Anode-Layer Type Hall Thruster, 27th International Symposium on Space Technology and Science, ISTS2009-b-60b, USB-flash-disk (5 pages) , Tsukuba, Japan, July, 2009.
[26] S. Cho, S. Yokota, K. Hara, D. Takahashi, Y. Arakawa, K. Komurasaki, and A. Kobayashi, Development of Lifetime Evaluation Method Using Multilayer Coating Chip, 27th International Symposium on Space Technology and Science, ISTS2009-b-43s, USB-flash-disk (3 pages), Tsukuba, Japan, July, 2009.
[25] S. Cho, S. Yokota, Y. Fukushima, K. Hara, Y. Arakawa, K. Komurasaki, and A. Kobayashi, Application of Lifetime Evaluation Method Using Multilayer Coated Chips, Proceedings of 16th Annual Meeting of IAPS, p. 84, Kobe, March, 2009.
[24] Yokota, S., Lempke, M., Matsui, M., Hara, K., Komurasaki, K., Arakawa, Y., “Diagnostics of Xe Ion in an Anode-layer Type Hall Thruster Using Laser Induced Fluorescence,” International Symposium on Space Technology and Science, ISTS2008-b-22, Hamamatsu, 2008.
[23] Fukushima, Y., Yokota, S., Komurasaki, K., Arakawa, Y., “Oscillation Reduction of an Anode- Layer- Type Hall Thruster by Azimuthal Propellant Nonuniformity.” 44th AIAA/ASME/SAE/ASEE Joint Propulsion Conference & Exhibit, AIAA2008-5187, Hartford, CT, Jul., 2008.
[22] Lempke, M., Yokota, S., Matsui, M., Hara, K., Komurasaki, K., and Arakawa, Y., "LIF Spectroscopy of a Hall Thruster Plasma Plume," 15th Annual Meeting of Institute of Applied Plasma Science, C-1, Dalian, China, March, 2008.
[21] Yokota, S., Fukushima, Y., Tsukizaki, R., Komurasaki, K., and Arakawa, Y., Kobayashi, A., " Development of Hall Thruster Life Time Measurement Method Using Multilayer Coated Chip," 15th Annual Meeting of Institute of Applied Plasma Science, P-3, Dalian, China, March, 2008.
[20] Yokota, S., Komurasaki, K., and Arakawa, Y., " Numerical Analysis of Anode Sheath Structure Shift in an Anode-layer Type Hall Thruster," 47th Asian Joint Conference in Propulsion and Power, AJCPP2008-C6-5,March 6-8, 2008, Gyeongju, Korea
[19] Fukushima, Y., Yokota, S., Komurasaki, K., and Arakawa, Y., " Thrust Vector Control and Discharge Stabilization in a Hall Thruster by Azimuthal Division of Propellant Flow Rate," 47th Asian Joint Conference in Propulsion and Power, AJCPP2008-C5-4,March 6-8, 2008, Gyeongju, Korea
[18] Sakoh, D., Yokota, S, Komurasaki, K., Arakawa, Y., “Charge Exchanged Ions in a Hall Thruster Plasma Plume,” International Symposium on Applied Plasma Science 2007, P-II-5, Sep., 2007.
[17] M. Matsui, S. Yokota, D. Sakoh, K. Komurasaki, Y. Arakawa, "Distribution of Unionized Propellant Xenon in a Hall Thruster Plum," 30th International Electric Propulsion Conference, IEPC2007-46, Florence, Italy, Sep. 17-20, 2007.
[16] N. Takahashi, N. Yamamoto, S. Yokota, K. Komurasaki, H. Nakashima, Y. Arakawa, "Investigation of Internal Plasma Structure in an Anode-Layer Hall Thruster," 30th International Electric Propulsion Conference, IEPC2007-92, Florence, Italy, Sep. 17-20, 2007.
[15] S., Yokota, K., Komurasaki, Y., Arakawa, "Numerical Analysis of Anode Sheath Structure Transition in an Anode-Layer Type Hall Thruster," 30th International Electric Propulsion Conference, IEPC2007-95, Florence, Italy, Sep. 17-20, 2007.
[14] Matsui, M., Yokota, S., Sakoh, D., Komurasaki, K., and Arakawa, Y., "Number Density Distributions of Xenon Atom in Hall Thruster Plumes," 43rd AIAA/ASME/SAE/ASEE Joint Populsion Conference & Exibit, AIAA2007-5298, Cincinnati, OH, Jul., 2007.
[13] Nagao, N., Yokota, S., Komurasaki, K., and Arakawa, Y., "Development of a Dual Pendulum Thrust Stand for Hall Thrusters," 43rd AIAA/ASME/SAE/ASEE Joint Populsion Conference & Exibit, AIAA2007-5298, Cincinnati, OH, Jul., 2007.
[12] Yokota, S., Komurasaki, K., and Arakawa, Y., "Numerical Analysis in an Anode-Layer-Type Hall Thruster," The 3rd International Symposium on Inovative Aerial/Space Flyer Systems, P-19, Tokyo, Nov., 2006.
[11] Yokota, S., Komurasaki, K., and Arakawa, Y., "Plasma Density Fluctuation inside a Hollow Anode in an Anode-layer Hall Thruster," 42nd AIAA/ASME/SAE/ASEE Joint Populsion Conference & Exibit, AIAA2006-5170, Sacrament, CA, Jul., 2006.
[10] Yokota, S., Matsui, M., Sako, D., Yamamoto, N., Koizumi, H., Komurasaki, K., Nakashima, H., and Arakawa, Y., "Diagnostics of Hall Thruster Plume by Laser Absorption Spectroscopy," 42nd AIAA/ASME/SAE/ASEE Joint Populsion Conference & Exibit, AIAA2006-5028, Sacrament, CA, Jul., 2006.
[9] Yokota, S., Matsui, M., Sako, D., Nagao, N., Takayanagi, H., Koizumi, H., Komurasaki, K. and Arakawa, Y., "Laser Diagnostics of Xenon Atom in Hall Thruster Plume," International Symposium on Space Technology and Science, ISTS 2006-b-51p, Kanazawa, Jun., 2006.
[8] Yokota, S., Komurasaki, K., Arakawa, Y., "The Fluctuation of Electron Density Distribution Inside a Hollow Anode in an Anode-Layer Hall Thruster," 25th International Symposium on Space Technology and Science, ISTS2006-b37, Kanazawa, Jun,, 2006.
[7] Yokota, S., Komurasaki, K., Arakawa, Y., "Plasma Profile on the Oscillation Mode inside a Hollow Anode of Anode-Layer Hall Thruster," 46th Asian Joint Conference in Propulsion and Power, AJCPP2006-J1015, Beijing, Apr., 2006.
[6] Matsui, M., Yokota, S., Yamamoto, N., Koizumi, H., Komurasaki, K. Nakashima, H., and Arakawa, Y., "Xenon Density Measurement of Hall Thruster Plume by Laser Absorption Spectroscopy," Spectra Asia, Tokyo, May, 2006.
[5] Matsui, M., Yokota, S., Takayanagi, H., Koizumi, H., Komurasaki, K. and Arakawa, Y., "Plume Characterization of Plasma Thrusters using Diode Laser Absorption Spectroscopy," 44th AIAA Aerospace Sciences Meeting and Exhibit, AIAA Paper 06-0767, Reno, Jan., 2006.
[4] N., Yamamoto, S., Yokota, M., Matsui, K., Komurasaki, Y., Arakawa, "Measurement of Erosion Rate by Absorption Spectroscopy in a Hall Thruster" 29th International Electric Propulsion Conference, IEPC2005-037, Princeton University, Oct., 2005.
[3] S., Yokota, K., Komurasaki, Y., Arakawa, "Space Potential Fluctuation in an Anode-Layer Hall Thruster," 29th International Electric Propulsion Conference, IEPC2005-124, Princeton University, Oct., 2005.
[2] S., Yokota, S., Yasui, K., Komurasaki, Y., Arakawa, "Plasma Instability Inside a Hollow Anode of Anode-Layer Hall Thruster," 45th Asian Joint Conference in Propulsion and Power, AJCPP2005-22062, Kitakyushu, Jan., 2005.
[1] K., Komurasaki, S., Yokota, S., Yasui, and Y., Arakawa, "Particle Simulation of Plasma Dynamics Inside an Anode-Layer Hall Thruster," 40th AIAA/ASME/SAE/ASEE Joint Propulsion Conference and Exhibit, AIAA2004-3945, Fort Lauderdale, Florida, Jul., 2004

 

 

国内発表

[37] 長谷川直紀, 横田茂, 佐宗章弘, 2波長単一結像マッハツェンダ干渉法を用いた電離流れの計測, 平成24年度衝撃波シンポジウム, 北九州, 2013年3月.
[36] 市原大輔, 原田翔太, 横田茂, 佐宗章弘, 永久磁石を用いた定常・外部磁場印加型MPDスラスタの作動特性, 平成24年度宇宙輸送シンポジウム, ISAS/JAXA, 2013年3月.
[35] 鶴田久, 横田茂, 佐宗章弘, アルミニウムに対する繰り返しパルス照射による レーザーアブレーションの力積特性, 平成24年度宇宙輸送シンポジウム, ISAS/JAXA, 2013年3月.
[34] 市原大輔, 原田翔太, 横田茂, 佐宗章弘, 大電力化に向けた定常・外部磁場印加型MPDスラスターの開発, 第56回宇宙科学技術連合講演会, 別府, 2012年11月.
[33] 横田茂, 張科寅, 高橋大輔, 小紫公也, 荒川義博, アノードレイヤ型ホールスラスタの作動安定化, プラズマパルスパワー合同研究会, 岩手, 2012年8月.
[32] 山本直嗣, 横田茂, 小紫公也, 5kW級アノードレーヤー型ホールスラスタの設計とさらなる大型化への指針, 第56回宇宙科学技術連合講演会, 別府, 2012年11月.
[31] 市原大輔, 原田翔太, 横田茂, 佐宗章弘, 高インピーダンス MPD スラスタの作動特性,第49回日本航空宇宙学会中部・関西支部合同秋期大会, 名古屋, 2012年11月.
[30] 鶴田久, 横田茂, 佐宗章弘, 高繰返しパルスレーザー照射時におけるアルミニウムのアブレーション力積特性, 第49回日本航空宇宙学会中部・関西支部合同秋期大会, 名古屋, 2012年11月.
[29] 市原大輔, 原田翔太, 横田茂, 佐宗章弘, ホローカソードを用いた矩形形状MPDスラスタの性能評価, プラズマパルスパワー合同研究会, 岩手, 2012年8月.
[28] 竹矢憲司, 横田茂, 佐宗章弘, 衝撃波管内における繰り返しレーザーパルスによる低密度バブル列の形成, 平成23年度衝撃波シンポジウム, 東京大学, 2012年3月.
[27] 長谷川直紀, 米元聖貴, 横田茂, 酒井武治, 佐宗章弘, 単一画面結像2波長マッハツェンダ干渉法を用いた電子-重粒子密度場の同時計測,平成23年度衝撃波シンポジウム, 東京大学, 2012年3月.
[26] 山本直嗣, 宮坂武志, トニーショーンヘル, 横田茂, 尾崎敏之, 大須賀弘行, 田原弘一, 小紫公也, 小泉宏之, 船木一幸, In Space Propulsionとしての大型ホールスラスタの検討, 平成23年度宇宙輸送シン ポジウム, ISAS/JAXA, 2012年1月.
[25] 原田翔太, 横田茂, 佐宗章弘, 鶴田久, アルミニウム表面への高繰返しレーザーパルス照射における力積特性, 平成23年度宇宙輸送シンポジウム, ISAS/JAXA , 2012年1月.
[24] 市原大輔, 榎伯仁, 横田茂, 佐宗章弘, 定常・外部磁場印加型・矩形加速領域MPDスラスタの作動特性, 平成23年度宇宙輸送シンポジウム, ISAS/JAXA , 2012年1月.
[23] 榎伯仁, 市原大輔, 横田茂, 佐宗章弘, 誘導結合プラズマを用いた回転磁場型無電極電気推進機の試作, 平成23年度宇宙輸送シンポジウム, ISAS/JAXA, 2012年1月.
[22] 市原大輔, 榎伯仁, 横田茂, 佐宗章弘, ホローカソードを用いた2次元MPDスラスタの性能評価, 第55回宇宙科学技術連合講演会, 愛媛, 2011年11月.
[21] 張科寅, 横田茂, 金子亮太郎, 細田誠也, 小紫公也, 荒川義博, 粒子法を用いた小型ホールスラスタの放電シミュレーション, 第55回宇宙科学技術連合講演会, 愛媛, 2011年11月.
[20] 神谷勇多, 酒井武治, 山下聖主, 横田茂, 佐宗章弘, 繰り返しパルスエネルギー付加による超音速飛行物体の空力特性, 第43回流体力学講演会/航空宇宙数値シミュレーション技術シンポジウム, 早稲田大学, 2011年7月.
[19] 高橋大祐,横田茂,張科寅,金子亮太郎,細田誠也,荒川義博,小紫公也,ホールスラスタ表面の絶縁体被覆によるイオン損失低減, 平成23年度宇宙輸送シンポジウム, ISAS/JAXA, 2011年1月.
[18] 張科寅,横田茂,高橋大祐,金子亮太郎,荒川義博,小紫公也, 小型ホールスラスタの推進性能及び壁面損耗評価, 平成22年度宇宙輸送シンポジウム, ISAS/JAXA, 2011年1月.
[17] Schoenherr Tony,小紫公也,川島嶺,横田茂,荒川義博,Lau, Matthias,Herdrich, Georg,Roeser, Hans-Peter,SIMP-LEX - A German-Japanese Pulsed Plasma Thruster Project,平成21年度宇宙輸送シンポジウム,STEP-2009-36,相模原,2010年1月.
[16] 横田茂, 原健太郎, 張科寅, 高橋大祐, 小紫公也, 荒川義博,ホールスラスタ内部のプラズマ-壁面間相互干渉の数値解析,第23回数値流体力学シンポジウム,E9-2,仙台,2009年12月.
[15] 原健太郎,横田茂,張科寅,小紫公也,荒川義博,ホールスラスタ壁面効果に関する数値解析,第53回宇宙科学技術連合講演会,1K09,京都,2009年9月.
[14] 横田茂,原健太郎,張科寅,小紫公也,荒川義博,粒子法を用いたアノードレイヤ型ホールスラスタ陽極近傍の数値解析,日本航空宇宙2007学会第40期年会講演会,C02,調布,2009年4月.
[13] 原健太郎,横田茂,福島靖博,張科寅,小紫公也,荒川義博,二次電子放出が及ぼすホールスラスタ壁面シースへの影響と数値解析,日本航空宇宙学会第40期年会講演会,B16,調布,2009年4月.
[12] 月崎竜童,横田茂,福島靖博,小紫公也,荒川義博,小林明,“多層コーティングチップによるホールスラスタの寿命評価法,” 平成19年度宇宙輸送シンポジウム,宇宙科学研究所,2008年1月.
[11] 原健太郎,レンプケ・マルクス,横田茂,小紫公也,荒川義博,“レーザー誘起蛍光法によるホールスラスタ出口付近の速度成分計測,” 平成19年度宇宙輸送シンポジウム,宇宙科学研究所,2008年1月.
[10] 横田茂,小紫公也,荒川義博,“ホールスラスタ解析用粒子法コードの並列化,” 第47回航空原動機・宇宙推進講演会,姫路,2007年3月
[9] 山本直嗣,横田茂,中島秀紀,荒川義博, “ホールスラスタの内部診,” 第47回航空原動機・宇宙推進講演会,姫路,2007年3月
[8] 長尾直樹,横田茂,小紫公也,荒川義博, “2次元推力測定可能な2重振り子式スラストスタンドの開発,” 第47回航空原動機・宇宙推進講演会,姫路,2007年3月
[7] 長尾直樹,横田茂,小紫公也,荒川義博, “二重振り子式スラストスタンドの開発,” 平成18年度宇宙輸送シンポジウム,宇宙科学研究所,2007年1月
[6] 佐孝大地,松井信,横田茂,小泉宏之,小紫公也,荒川義博, “ホールスラスタプルームにおける中性粒子数密度分布計測,” 平成18年度宇宙輸送シンポジウム,宇宙科学研究所,2007年1月
[5] 横田茂,小紫公也,荒川義博, “アノードレイヤ型ホールスラスタのホローアノード内部の数値解析,” プラズマ応用科学代13回年会,福岡,2006年3月
[4] 井上孝祐,小泉宏之,田中佳介,横田茂, “誘導結合型プラズマを用いた無電極中和器,” 平成17年度宇宙輸送シンポジウム,宇宙科学研究所,2006年1月
[3] 長尾直樹,横田茂,佐孝大地,小泉宏之,小紫公也,荒川義博, “2重振り子式スラストスタンドの開発,” 平成17年度宇宙輸送シンポジウム,宇宙科学研究所,2006年1月
[2] 松井信,横田茂,佐孝大地,長尾直樹,高柳大樹,小泉宏之,小紫公也,荒川義博, “レーザー吸収分光法によるホールスラスタプルーム内のキセノン原子分布測定,” 平成17年度宇宙輸送シンポジウム, 宇宙科学研究所, 2006年1月
[1] 山本直嗣,横田茂,安井伸輔,小紫公也,荒川義博, “吸収分光法を用いたホールスラスタの寿命評価,” 平成16年度宇宙輸送シンポジウム,宇宙科学研究所,2004年1月