推進システムの長寿命化を目的とした磁場構造制御による推力方向制御手法の実証

[1] V.D. Kuznetsov, V.M. Sinelnikov, and S.N. Alpert. Yakov alpert: Sputnik-1 and the first satellite ionospheric experiment. Advances in Space Research, Vol. 55, No. 12, pp. 2833 – 2839, 2015.

[2] Jet Propulsion Laboratory. Mariner Mission to Venus. Jet Propulsion Laboratory, 2017.

[3] N. Oran W. A Review of the Mariner IV Results. National Aeronautics and Space Administration, 1967.

[4] C. F. Hall. Pioneer 10. Science, Vol. 183, No. 4122, pp. 301–302, 1974.

[5] T. G. Northrop, A. G. Opp, and J. H. Wolfe. Pioneer 11 saturn encounter. Journal of Geophysical Research: Space Physics, Vol. 85, No. A11, pp. 5651–5653, 1980.

[6] J. A. Dunne. Mariner 10 mercury encounter. Science, Vol. 185, No. 4146, pp. 141–142, 1974.

[7] E. C. Stone. The voyager 2 encounter with uranus. Journal of Geophysical Re- search: Space Physics, Vol. 92, No. A13, pp. 14873–14876, 1987.

[8] E. C. Stone and E. D. Miner. The voyager encounter with neptune. Journal of Geophysical Research: Space Physics, Vol. 96, No. S01, pp. 18903–18906, 1991.

[9] D. A. Gurnett, W. S. Kurth, L. F. Burlaga, and N. F. Ness. In situ observations of interstellar plasma with voyager 1. Science, Vol. 341, No. 6153, pp. 1489–1492, 2013.

[10] E. C. Stone, A. C. Cummings, B. C. Heikkila, and N. Lal. Cosmic ray measure- ments from voyager 2 as it crossed into interstellar space. Nature Astronomy, Vol. 3, No. 11, pp. 1013–1018, Nov 2019.

[11] I. Crawford. The scientific legacy of apollo. Astronomy & Geophysics, Vol. 53, No. 6, pp. 6.24–6.28, 2012.

[12] David M Harland. The story of space station MIR. Springer Science & Business Media, 2007.

[13] GH Kitmacher. Reference guide to the International Space Station: Assembly com- plete edition. CreateSpace Independent Publishing, Charleston/SC, USA, 2010.

[14] Y. Suzuki, K. Tsuchida, Y. Matsusaki, A. Hashimoto, S. Tanaka, T. Ikeda, and N. Okumura. Performance evaluation of transmission system for 8k super hi- vision satellite broadcasting. In 2014 IEEE Global Communications Conference, pp. 2886–2891, 2014.

[15] P. K. Rao, S. J. Holmes, R. K. Anderson, J. S. Winston, and P. E. Lehr. Weather satellites: Systems, data, and environmental applications. Springer Nature, 1990.

[16] J. J. Spilker Jr., P. Axelrad, B. W. Parkinson, and P. Enge. Global Positioning System: Theory and Applications. American Institute of Aeronautics and Astro- nautics, 1996.

[17] J. Foust. Gateway or bust: Nasa’s plan for a 2024 lunar landing depends on a much-criticized orbital outpost. IEEE Spectrum, Vol. 56, No. 7, pp. 32–37, 2019.

[18] Owen Gwynne, Yoji Ishikawa, Yukinobu Yamamoto, Hisateru Uyeda, and Thomas Bongiovi. Construction and development of a human base on mars. En- gineering, Construction, and Operations in space-III: Space’92, Vol. 1, pp. 89–99, 1992.

[19] John S Lewis. Asteroid mining 101: wealth for the new space economy. Deep Space Industries, 2015.

[20] Alan W. H. and L. Drube. HOW TO FIND METAL-RICH ASTEROIDS. The Astrophysical Journal, Vol. 785, No. 1, p. L4, mar 2014.

[21] J. R. Johnson, T. D. Swindle, and P. G. Lucey. Estimated solar wind-implanted helium-3 distribution on the moon. Geophysical Research Letters, Vol. 26, No. 3, pp. 385–388, 1999.

[22] Luxembourg. Loi du 20 juillet 2017 sur l’exploration et l’utilisation des ressources de l’espace, 2017.

[23] A. P. Vinogradov. Preliminary data on the lunar soil brought to earth by auto- matic probe" luna 16". JBIS, Vol. 24, pp. 475–495, 1971.

[24] S. Watanabe, Y. Tsuda, M. Yoshikawa, S. Tanaka, T. Saiki, and S. Nakazawa. Hayabusa2 mission overview. Space Science Reviews, Vol. 208, No. 1, pp. 3–16, Jul 2017.

[25] W. Johnson. Contents and commentary on william moore’s a treatise on the mo- tion of rockets and an essay on naval gunnery. International Journal of Impact Engineering, Vol. 16, No. 3, pp. 499 – 521, 1995.

[26] A. Kosmodemyansky and X. Danko. Konstantin Tsiolkovsky: His Life and Work. The Minerva Group, Inc., 2000.

[27] R. H. Goddard. A method of reaching extreme altitudes. Nature, Vol. 105, No. 2652, pp. 809–811, Aug 1920.

[28] W. A.SS Mrazek. The saturn v launch vehicle. Technical report, SAE Technical Paper, 1964.

[29] T. Ito, T. Yamamoto, T. Nakamura, H. Habu, and H. Ohtsuka. Sounding rocket ss-520 as a cubesat launch vehicle. Acta Astronautica, Vol. 170, pp. 206–223, 2020.

[30] E. Seedhouse. Falcon 9 and falcon heavy: Life after the space shuttle. In SpaceX, pp. 65–84. Springer, 2013.

[31] E. Y. Choueiri. A critical history of electric propulsion: The first 50 years (1906- 1956). Journal of Propulsion and Power, Vol. 20, No. 2, pp. 193–203, 2004.

[32] R. J. Cybulski, D. M. Shellhammer, R. R. Lovell, E. J. Domino, J. T. Kotnik, J. Cy- bulski, and R. R. Loveli. Results from sert i ion rocket flight test. In Proceedings, Vol. 1, p. 21. Air Force Office of Scientific Research, 1965.

[33] H. Kuninaka, K. Nishiyama, I. Funaki, T. Yamada, Y. Shimizu, and J. Kawaguchi. Powered flight of electron cyclotron resonance ion engines on hayabusa explorer. Journal of Propulsion and Power, Vol. 23, No. 3, pp. 544–551, 2007.

[34] BOEING. 702sp satellite, 2020. https://rsdo.gsfc.nasa.gov/images/ catalog/301406_RapidIII_4Page_Layout_A_REV_1_11.pdf.

[35] E. Canuto and L. Massotti. All-propulsion design of the drag-free and attitude control of the european satellite goce. Acta Astronautica, Vol. 64, No. 2, pp. 325 – 344, 2009.

[36] J. THIRKILL. Solid rocket motor for the space shuttle booster. In 11th Propulsion Conference, p. 1170, 1975.

[37] Y. Morita, T. Imoto, S. Tokudome, and H. Ohtsuka. Epsilon rocket launcher and future solid rocket technologies. TRANSACTIONS OF THE JAPAN SOCIETY FOR AERONAUTICAL AND SPACE SCIENCES, AEROSPACE TECHNOLOGY JAPAN, Vol. 10, No. ists28, pp. Tg_19–Tg_24, 2012.

[38] S. Jayaram, L. Boyer, J. George, K. Ravindra, and K. Mitchell. Project-based introduction to aerospace engineering course: A model rocket. Acta Astronautica, Vol. 66, No. 9, pp. 1525–1533, 2010.

[39] Y. Fukushima, H. Nakatsuzi, R. Nagao, K. Kishimoto, K. Hasegawa, T. Ko- ganezawa, and S. Warashina. Development status of le-7a and le-5b engines for h-iia family. Acta Astronautica, Vol. 50, No. 5, pp. 275–284, 2002.

[40] H. Nagata, M. Ito, T. Maeda, M. Watanabe, T. Uematsu, T. Totani, and I. Kudo. Development of camui hybrid rocket to create a market for small rocket experi- ments. Acta Astronautica, Vol. 59, No. 1, pp. 253–258, 2006. Space for Inspiration of Humankind, Selected Proceedings of the 56th International Astronautical Fed- eration Congress, Fukuoka, Japan, 17-21 October 2005.

[41] R. G. Jahn. Electric propulsion. American Scientist, Vol. 52, No. 2, pp. 207–217, 1964.

[42] O. Mori, H. Sawada, R. Funase, M. Morimoto, T. Endo, T. Yamamoto, Y. Tsuda, Y. Kawakatsu, J. Kawaguchi, Y. Miyazaki, Y. Shirasawa, IKAROS Demonstration Team, and Solar Sail Working Group. First solar power sail demonstration by ikaros. Transactions of the Japan Society for Aeronautical and Space Sciences, Aerospace Technology Japan, Vol. 8, No. ists27, pp. To_4_25–To_4_31, 2010.

[43] Y. Okawa, S. Kitamura, S. Kawamoto, Y. Iseki, K. Hashimoto, and E. Noda. An ex- perimental study on carbon nanotube cathodes for electrodynamic tether propul- sion. Acta Astronautica, Vol. 61, No. 11, pp. 989–994, 2007.

[44] R. G. Jahn. Physics of electric propulsion. Courier Corporation, 2006.

[45] W. Birk, L. Q. Hoa, and G. Herdrich. Overview of thermal arcjet thruster de- velopment. Aircraft Engineering and Aerospace Technology, Vol. 90, No. 2, pp. 280–301, Jan 2018.

[46] J. Asakawa, H. Koizumi, K. Nishii, N. Takeda, M. Murohara, R. Funase, and K. Komurasaki. Fundamental ground experiment of a water resistojet propulsion system: Aquarius installed on a 6u cubesat: Equuleus. Transactions of the Japan Society for Aeronautical and Space Sciences, Aerospace Technology Japan, Vol. 16, No. 5, pp. 427–431, 2018.

[47] J. R. Brophy. Nasa ’s deep space 1 ion engine (plenary). Review of Scientific Instruments, Vol. 73, No. 2, pp. 1071–1078, 2002.

[48] Y. Hamada, J. Bak, R. Kawashima, H. Koizumi, K. Komurasaki, N. Yamamoto, Y. Egawa, I. Funaki, S. Iihara, S. Cho, K. Kubota, H. Watanabe, K. Fuchigami, Y. Tashiro, Y. Takahata, T. Kakuma, Y. Furukubo, and H. Tahara. Hall thruster development for japanese space propulsion programs. TRANSACTIONS OF THE JAPAN SOCIETY FOR AERONAUTICAL AND SPACE SCIENCES, Vol. 60, No. 5, pp. 320–326, 2017.

[49] T. Yoshikawa, Y. Kagaya, and K. Kuriki. Thrust and efficiency of the k-iii mpd thruster. Journal of Spacecraft and Rockets, Vol. 21, No. 5, pp. 481–487, 1984.

[50] D. Kuwahara, S. Shinohara, and K. Yano. Thrust characteristics of high-density helicon plasma using argon and xenon gases. Journal of Propulsion and Power, Vol. 33, No. 2, pp. 420–424, 2017.

[51] A. A. Blagonravov, B. N. Yuryev, B. A. Semenov, A. A. Komodemyanskiy, M. K. Tikhonravov, and B. N. Vorobyev. Collected works of k. e. tsiolkovskiy vol ii reac- tive flying machines. NASA Technical Translation, Vol. F-237, , 1954.

[52] MHI LAUNCH SERVICES. H-iia user’s manual ver 4.0, 2015.

[53] Y. Tani, R. Tsukizaki, D. Koda, K. Nishiyama, and H. Kuninaka. Performance improvement of the μ 10 microwave discharge ion thruster by expansion of the plasma production volume. Acta Astronautica, Vol. 157, pp. 425–434, 2019.

[54] A Stanculescu. The role of nuclear power and nuclear propulsion in the peaceful exploration of space, Vol. 1197. IAEA, 2005.

[55] Francis de Winter, Gerhard Stapfer, and Enrique Medina. The design of a nuclear power supply with a 50 year life expectancy: the jpl voyager ’s sige mhw rtg. Technical report, SAE Technical Paper, 1999.

[56] Mohamed S El-Genk. Deployment history and design considerations for space reactor power systems. Acta Astronautica, Vol. 64, No. 9-10, pp. 833–849, 2009.

[57] Eugene V Pawlik and Wayne M Phillips. A nuclear electric propulsion vehicle for planetary exploration. Journal of Spacecraft and Rockets, Vol. 14, No. 9, pp. 518–525, 1977.

[58] CD Orth. Vista-a vehicle for interplanetary space transport application powered by inertial confinement fusion. University of California, Lawrence Livermore Na- tional Laboratory, Report UCRL-LR-110500, in final preparation, 2003.

[59] Craig H Williams, Leonard A Dudzinski, Stanley K Borowski, and Albert J Juhasz. Realizing" 2001: A space odyssey": Piloted spherical torus nuclear fu- sion propulsion. Journal of spacecraft and rockets, Vol. 39, No. 6, pp. 874–885, 2002.

[60] Yoshihiro Kajimura, Ryo Kawabuchi, and Hideki Nakashima. Control techniques of thrust vector for magnetic nozzle in laser fusion rocket. Fusion engineering and design, Vol. 81, No. 23-24, pp. 2871–2875, 2006.

[61] Mario Merino and Eduardo Ahedo. Contactless steering of a plasma jet with a 3d magnetic nozzle. Plasma Sources Science and Technology, Vol. 26, No. 9, p. 095001, aug 2017.

[62] Y Kajimura, R Kawabuchi, N Matsuda, and H Nakashima. Numerical simulation of fusion plasma behavior in a magnetic nozzle for laser fusion rocket. Fusion science and technology, Vol. 51, No. 2T, pp. 229–231, 2007.

[63] N. Matsuda, A. Maeno, Y. Kajimura, and H. Nakashima. A magnetic thrust chamber design for a laser fusion rocket based on impact fast ignition scheme. J. Plasma Fusion Res. Series, Vol. 8, pp. 1602–1605, 2009.

[64] J. Brophy. The dawn ion propulsion system. Space Science Reviews, Vol. 163, No. 1, pp. 251–261, Dec 2011.

[65] W. R. Jones Jr and M. J. Jansen. Space tribology. NASA, No. TM-2000-209924, 2000.

[66] E. W. Roberts. Space tribology: its role in spacecraft mechanisms. Journal of Physics D: Applied Physics, Vol. 45, No. 50, p. 503001, nov 2012.

[67] Richard R Burt and Richard W Loffi. Failure analysis of international space station control moment gyro. In 10th European Space Mechanisms and Tribology Symposium, Vol. 524, pp. 13–25, 2003.

[68] A. Sunahara, K. Nishihara, and A. Sasaki. Optimization of extreme ultravio- let emission from laser-produced tin plasmas based on radiation hydrodynamics simulations. Plasma and Fusion Research, Vol. 3, pp. 043–043, 2008.

[69] A. Sunahara, T. Johzaki, H. Nagatomo, and K. Mima. Generation of pre-formed plasma and its reduction for fast-ignition. Laser and particle beams, Vol. 30, No. 01, pp. 95–102, 2012.

[70] R. C. Malone, R. L. McCrory, and R. L. Morse. Indications of strongly flux-limited electron thermal conduction in laser-target experiments. Physical Review Letters, Vol. 34, No. 12, p. 721, 1975.

[71] W. L. Kruer. The physics of laser plasma interactions. Addison-Wesley Publishing Co., 1988.

[72] L. Spitzer Jr. Physics of fully ionized gases:Second Revised Edition. Dover Publi- cations, 2006.

[73] L. Spitzer Jr and R. Härm. Transport phenomena in a completely ionized gas. Physical Review, Vol. 89, No. 5, p. 977, 1953.

[74] S. I. Braginskii. Transport processes in a plasma. Reviews of plasma physics, Vol. 1, p. 205, 1965.

[75] Y. Nagamine and H. Nakashima. Analysis of plasma behavior in a magnetic thrust chamber of a laser fusion rocket. Fusion Science and Technology, Vol. 35, No. 1, pp. 62–70, 1999.

[76] A. Mankofsky, R. N. Sudan, and J. Denavit. Hybrid simulation of ion beams in background plasma. Journal of Computational Physics, Vol. 70, No. 1, pp. 89–116, 1987.

[77] T. Bagdonat and U. Motschmann. 3d hybrid simulation code using curvilinear coordinates. Journal of Computational Physics, Vol. 183, No. 2, pp. 470–485, 2002.

[78] C. G. Darwin. Li. the dynamical motions of charged particles. The London, Edin- burgh, and Dublin Philosophical Magazine and Journal of Science, Vol. 39, No. 233, pp. 537–551, 1920.

[79] M. Edamoto, N. Saito, T. Morita, N. Yamamoto, S. Miura, Y. Itadani, T. Kojima, H. Nakashima, A. Sunahara, S. Fujioka, A. Yogo, H. Nishimura, Y. Mori, and T. Johzaki. Parametric numerical analysis of plasma behaviors in a magnetic nozzle for a laser fusion rocket. In 35th International Electric Propulsion Confer- ence, Atlanta, Georgiam USA, pp. IEPC–2017–452, 2017.

[80] N. Saito, N. Yamamoto, T. Morita, M. Edamoto, H. Nakashima, S. Fujioka, A. Yogo, H. Nishimura, A. Sunahara, Y. Mori, and T. Johzaki. Experimental demonstration of ion extraction from magnetic thrust chamber for laser fusion rocket. Japanese Journal of Applied Physics, Vol. 57, No. 5, p. 050303, mar 2018.

[81] M. Edamoto, A. Sunahara, T. Morita, N. Saito, Y. Itadani, T. Kojima, M. Tak- agi, S. Fujioka, A. Yogo, H. Nishimura, Y. Mori, T. Johzaki, H. Nakashima, and N. Yamamoto. Numerical simulation of the plasma control method using a diver- gent magnetic field for a laser fusion rocket. In Plasma Conference 2017, Himeji, Japan, pp. 22Gp–05, 2017.

[82] M. Edamoto, N. Saito, T. Morita, N. Yamamoto, A. Sunahara, R. Kawashima, S. Miura, Y. Itadani, H. Nakashima, S. Fujioka, A. Yogo, H. Nishimura, Y. Mori, and Johzaki T. Development of a magnetic thrust chamber for a laser fusion rocket. In 52nd AIAA/SAE/ASEE Joint Propulsion Conference, p. 4684, 2016.

[83] T. Morita, M. Edamoto, S. Miura, A. Sunahara, N. Saito, Y. Itadani, T. Ko- jima, Y. Mori, T. Johzaki, Y. Kajimura, S. Fujioka, A. Yogo, H. Nishimura, H. Nakashima, and N. Yamamoto. Control of unsteady laser-produced plasma- flow with a multiple-coil magnetic nozzle. Scientific reports, Vol. 7, No. 1, pp. 1–7, 2017.

[84] Y. Kajimura, R. Kawabuchi, N. Matsuda, and H. Nakashima. Numerical simula- tion of fusion plasma behavior in a magnetic nozzle for laser fusion rocket. Fusion Science and Technology, Vol. 51, No. 2T, pp. 229–231, 2007.

[85] M. Edamoto, T. Morita, N. Saito, Y. Itadani, S. Miura, S. Fujioka, H. Nakashima, and N. Yamamoto. Portable and noise-tolerant magnetic field generation system. Review of Scientific Instruments, Vol. 89, No. 9, p. 094706, 2018.

[86] 林 泉, 中野 義映. ロゴスキーコイルと磁気探針. 電氣學會雜誌, Vol. 81, No. 874, pp. 1084–1092, 1961.

[87] 天岸祥光. 6. 磁気プローブ, ループでプラズマを探る. プラズマ・核融合学会誌, Vol. 69, No. 10, 1993.

[88] 大阪大学レーザー科学研究所. 激光XII 号, 最終閲覧日: 2021 年07 月23 日. https://www.ile.osaka-u.ac.jp/ja/facilities/gxii/index.html.

[89] T. Morita, N. Yamamoto, R. Kawashima, N. Saito, M. Edamoto, S. Fujioka, Y. Itadani, T. Johzaki, S. Miura, Y. Mori, H. Nishimura, A. Sunahara, A. Yogo, and H. Nakashima. Plasma structure and energy dependence in a magnetic thrust chamber system. Journal of Physics: Conference Series, Vol. 717, No. 1, p. 012071, 2016.

[90] S. Yoshimura, K. Terasaka, Y. Kato, M. Aramaki, and M.Y. Tanaka. 2d measure- ment of field-aligned intermittent high-energy electron flux in an ecr discharge plasma. Vol. 2, pp. 1094–1097, 2012.