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PROCEEDINGS of the TWENTY-FIFTH INTERNATIONAL SYMPOSIUM on SPACE TECHNOLOGY and SCIENCE ( Selected Papers )

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PROCEEDINGS OF THE TWENTY-FIFTH INTERNATIONAL SYMPOSIUM ON SPACE TECHNOLOGY AND SCIENCE ( Selected Papers ) KANAZAWA 2006 JSASS and ISTS CONTENTS-.•••.— .—••. •-.•-. Title/Authors ,!T,;, Paper No. Page Development and Results of Space Evaluation Test for Vane Type Tank 2006-a-02 1 System(VTS)- - • ' - .-.-i s--»'o-. : .•;-..:-,,-i::v».3C.; lo f-:;jiiij,,<:"i Ryoji Imai, Yosuke Takano, Keisuke Yamada, Kazunor Hama, Shuji Nakamura '•- -i'-:y:••--'. K: ,: < "irki f ,»!rna>i ii;;ii.r:?t> • Experimental Investigation of the Dynamic Characteristics of Lateral Liquid <•) c2006-a-03>*J ;in;i>K6; Sloshing in a Concentric Membrane Tank ix?/iHn>rtV M:r, <:V.-"V; -.: -r, ;;,: ir.ciiqr!'1. - Keiji Komatsu, Miki Nishimoto • ' • ' ''' . <""i •.".• i^an'. ,o."-.. '.=u-..-. i.-i-'...r.;! i, r ,.,.,,;. :'«:;.'J! .viiiii3Li!.«i Numerical Analysis of Dynamic Behavior of Free-Surface Flows in Tanks 2006-a-04 13 Based on CIPH.SM -'••: -V^' '•• -^ • •"' •- " ' •'•• ••-t- :,••>::,:.-••--h^; Hideyo Negishi, Takehiro Himeno, Nobuhiro Yamanishi : r '-.' - ":?.«.• Development of Numerical Methods for Propellant Management 2006-a-06 19 Takehiro Himeno, Toshinori Watanabe, Ryoji Imai •'•••" ' '"-'•'•'• -'' Cryogenic Propellant Management of H- IIA Upper Stage 2006-a-08 29 Osamu Kitayama, Iwao Igarashi, Tatsuru Tokunaga, Koichi Okita, Masumi Fujita Characteristics of Flows and Discharge Coefficients in Coaxial Injectors with 2006-a-13 '35 Cold Flow Tests Yoshio Nunome, Hiroshi Sakamoto, Takuo Onodera, Hiroshi Tamura, Takao Inamura, Akinaga Kumakawa •' ' ; ' ' Performance Evaluations of the Methane Fueled Rocket Nozzles under High 2006-a-18 41 Altitude Conditions . " . : Takashi Ito, Akinaga Kumakawa, Keiichi Hasegawa, Masaki Sato, Shinichi Moriya, Kazuo Kusaka, Masahiro Sato, Makoto Tadano . ... • . .. ... Flow Separation and the Associated Side-Load Origin in a Thrust Optimized 2006-a-2Q , 47, Parabolic Nozzle Shashi Verma, Oskar, Haidn . , ••,',.- ,-. :'••:''•• - . -.. : Survey of U.S. Small Launch Vehicle Failures ;2Q06Ta-22. ,,, 53 Edmardo Tomei, I-Shin Chang Survey of Non-U.S. Small Launch Vehicle Fai!ures\ 2QQ6-a-23 -, 63 I-Shih Chang, E Tomei High-Fidelity Simulation of Solid Propeliant Rockets 2006-a-27 • ••, :. 12 William Dick, Robert Fiedler, Michael Heath ,, ...... %. ^. ;,j SP Rocket Simulations at CSAR,,, ;J . .. -. o^ , 2006-aT28 t -i s 78i William Dick, Michael'Heath ' ' --.sjeuif!7* Combustion Characteristics of HAN-Based Liquid Monopropellant 2006-8-37 84 Toshiyuki Katsumi, Kenji.Hisatsune, Tetsuya Matsuo, Hidefumi,-Shibampto,.KeiichirHori;..v,-.'. ,., " •• ic.f -»-*'*:•' •' .sail--. i\l* ;','••; /-; Combustion Mechanism of Tetra-OI Glycidyl Azide Polymer , 2006-a-41 89 Yutaka Wada, Makito Nishioka, Keiichi Hori Design Study on Pre-Cooled Turbojet Engines for Hypersonic Airplanes 2006-a-43 95 Hideyuki Taguchi,*Takayuki Kojima, Kazuhisa Fujita, Hiroaki Kobayashi, Keiichi Okai, Tetsuya Sato'•'- Evaluate of Boundary Layer Introduced Streamwise Vortices in Scramjet . , 2006-a-45 101 Combustor Using Quantitative Schlieren Method ' Shoji Sakaue, Takakage Arai, Tetsuro Morisaki. Tetsuji Sunami, Katsuhiro Itoh Transition of Combustion Modes in a Scramjet Engine 2006-a-46r r ; 107 Toshinori Kouchi, Tohru Mitani, Sadatake Tomioka, Shuichi Ueda • Scramjet Characteristics at Mypervelocity Condition over Mach 10 Flight : 2006-a-47- ,115 - Application of a Diverging Combustor i \ ' v... :'.'•' Masahiro Takahashi, Tomoyuki Komuro, Kazuo Sato, Masatoshi Kodera, Hideyuki Tanno, Katsuhiro Itoh Performance Comparison of Combined Fuel Injection Methods in a 2006-a-48 * > 121 Staged-Combustion Scramjet Engine Shuichi Ueda, Sadatake Tomioka, Toshinori Kouchi, Kan Kobayashi, Kenji Kudo, Kanenori Kato Aerodynamic Performance of the Combined-Cycle Engine Inlet in a Supersonic 2006-a-51 127 Region Kouichiro Tani, Takeshi Kanda, Kanenori Kato, Noboru Sakuranaka, Syuuichi Watanabe • •• . • • Preliminary Tests of Downstream Combustion Ramjet-mode in a Combined 2006-a-53 136 Cycle Engine; Combustor .-•>,- ..-:-; .]y ;.-,;,--•„•;"• ~\ •.:•_:,.-•.. \-.-<---j •• ,c = Kanenori Kato, Takeshi Kanda, Kan Kobayashi, Kenji Kudo, Atsuo Murakami Progress of Scramjet and Combined-Cycle Engine Research at JAXA 2006-a-54 142 Takeshi Kanda b ) Electric and Advanced Propulsion Effects of Multi-Nozzle Jets on Thrust-Performance Improvement of 2006-b-01 149 Micro-Arcjets Kosuke Onodera, Tsuyoshi Noda, Hideyuki Hbrisawa, Itsuro, Kimura ' ' ' •.>-.-.. Characteristics of DDNP Combustion for MEMS Rocket Application 2006b-03 155 Koji Takahashi, Takahiro Okada, Tatsuya Ikuta, Takashi Nishiyama, Kunihito Nagayama, Yoshinori Yamada; Yoshiaki Mitarai ' ' ' " A Laser Ignition Microthruster for Microspacecraft Propulsion 2006-b-05 161 Masakatsu Nakano.Hiroyuki Koizumi, Takayoshi Inoue, Masashi Watanabe, Yoshihiro Arak'awa •••- • • Research and Development of Compact Laser Ablative Thrusters for Small 2006-b-06 , 165 Satellites rJ ""'X-'• -::^ r^ \^U:iry< •.':<-,- .:• no;:, • .,.. ••.• • ,-t-:j-.-.,.^ Hikaru Maesato, Hirokazu Tahara Electromagnetic Acceleration Characteristics of a Laser-Electric Hybrid J 2d06-b-08 ", 1 171 Thrusters ; . • • Yusuke Sasaki, Koki Sasaki, Hideyuki Horisawa, Itsuro Kimura , , . A Multi Pulse Experiment of a Micrbwave^Beaming fhruster r ^ '-'~i rj>' 2006-b-6sI 177 Yasuhisa Oda, Kimiya Komurasaki, Koji Takahashi, Atsushi Kasugai, Keishi Sakamoto Numerical Analysis on Ignition and Formation of, Lasei—SupportedlDetonation 182 Wave in Axisymmetric Nozzle Using Thermal Non-Equilibrium .Model , • : . Hiroyuki Shiraishi Research and Development of High-Impulse Electrothermal Pulsed Plasma. 2006rb-13 188 Thrusters Toshiaki Edamitsu. Hirokazu Tahara R&D on Pulsed Plasma Thruster with Wide Thrust Performance 2006rb-14 194 Yukiya Kamishima, Junpei Iio, Junji Uezu, Masayuki Mukai, Haruki Takegahara,' . .•'..:; Takasi Wakizono, Mitsuteru Sugiki Use of Solid Chemical Propellants for Coaxial Pulsed Plasma Thrusters 2006-b-16 .200 Hideto Mashidori, Takeshi Tachibana. •.:•..,....• : Performance Characteristics of ian -Electrothermal Pulsed: Plasma Thruster 2006-b-18 206 with an Insulator-Rod-Arranged Cavity Hirokazu Sugihara, Toshiaki Edamitsu, Hirokazu Tahara A Preliminary Study on an ActiveX-controlled Thrust Stand for Thrust 2006-b-19 212 Variation Measurement . Akira Kakami, Ryoma Hiyamizu, Shinichiro Masaki, Takeshi Tachibana. • HAYABUSA Explorerlon-Driven in Deep (Space ; 2006-b-20 218 Hitoshi Kuninaka, Kazutaka Nishiyama, Ikko Funaki, Tetsuya Yamada, Yukio.Shimizu,. Jun' ichiro Kawaguchi Result of 16,000 hours Endurance Test on 20mN Class Xenon Ion Thruster 2006-b-21 224 forETS-VIII -.:,...•:.•• Toshiyuki Ozaki, Yasutaka Inanaga, Yukikazu Kasai, Takafumi Nakagawa, Miwa Igarashi, Takashi Itoh,:Ken-richi Kajiwara ;.., -• •-• • • •'. .,.-.••'• .. ,:..,'!.,,••.-.: . : . Overview and Research Status of the JAXA 150-mN Ion Engine , ..-.•.:, 2006-b^22 230 Yasushi Ohkawa, Yukio Hayakawa, Hideki Yoshida, Katsuhiro Miyazaki. Shoji Kitamura, ; [ Ken-ichi Kajiwar,a_, _ ]-i ,- <""'••" \: •••:•'"".." : • . ' '• "•.'•" . • . ••' ' \? Effect of Substrate on Sustained Arc between Electrodes : 2006-b^26 ^236 Kazuhiro Toyoda, LSon Levy Ground-Based Experiment of High-Voltage Electric Breakdown of Spacecraft 2006-b-27 242 Insulator Surface in Ambient Plasma Environment ; Kouji HorikawaMHirokazu^ahara ,, ,.'<••._.• r "• — •;-,_-;•;; ;.::;; ^c^r..:*C "'\"J !y '':'•"••• "•-<-'• •". "2 ':,'. •''••".' '•' Application of NuSPACE to the Spacecraft Environment Analysis 2006-b-28' 250 Masaki Okada, Hideyuki Usui, Yoshiharu Omura, Hiroko Ueda, Takeshi Murata, Tooru Sugiyama Magnetic Field Configuration Effects on Thrust Performance of Miniature * 2006-b-30 254 Microwave Discharge Ion Engine Takayuki Chikaoka, ShinyaKondo, Naoji:Yamamoto, Hideki Nakashima Yoshivuki Takao • ' "i. > Performance Improvement of the Microwave Discharge Ion Thruster (1 20 2006-b-32 ;y; Tatsuya Naka, Kazutaka Nishiyama, Hitoshi Kuninaka Experimental Demonstration of Microwave Discharge Ion Engineiwithi :•:.!•:. .-2006Lbi33'q '• -' M265 10,000sec Isp Hiroshi Hayashi, Hitoshi Kuninaka, Mengu Cho Development Status of High PowerXenon Hall Thruster of MELCO '• • 2006-b-34 270 Toshiyuki Ozaki, Yasutaka Inanaga, Takafumi Nakagawa; YukikazuKasai, Katsuaki Matsui Influence of Magnetic Field Topography and Discharge Channel Structure on 2006-b-36 276 Perormance "ofan Anode-Layer Hall Thruster" " ' - ; Seiro Yuge, Hirokazu Tahara The Fluctuation of Electron Density Distribution Inside a Hollow Anode in an 2006-b-37 282 Anode Layer Hall Thruster . J: !,.<•• ; :;r Shigeru Yokota, Kimiya Komurasaki, Yoshihiro Arakawa^ - ' . j- Performance Characterization for Various Electrode Geometries in an 2006-b-39 288 'Magneto-Plasma-Dynamic Thruster':'! - ~ • ' ' Daisuke Nakata, Kyoichiro Toki, Ikkoh Funaki, Yukio Shimizu, Hitoshi Kuninaka, Yoshihiro Arakawa Magnetic Nozzle Acceleration in a Fast-flbwihgPlasma for the VASIMR ; ;: 2006-b-42 292 Thruster Akira Ando, M. Shibata, Y. Kasashima, K. Hattori, M. Inutake Study of Electrodeless Plasma Production and Electromagnetic Acceleration: 2006-b-45 298 Kyoichiro Toki, Shunjiro Shinohara, Takao Tanikawa, Tohru Hada, Ikkoh Funaki, Konstantin Shamrai, Takashi Hashimoto, Kenji Makita, Yasushi Ikeda' •;''-••• •>' "—'• •!•-'' ''- MHD Analysis-of Magnetosphere around Magneto Plasma Sail "'• '• '••• "><'- ''"•'!••' 2006-b-47'- 304 v • „..!.-;.. .,. * - ' ... Hiroyuki Nishida, Hiroyuki OGAWA, Ikkoh Funaki, Yoshifumi Inatani - * ' ' '' ~>' ''•• <"'•'•'•• ) e.,t, - •• i. •'• '• •••- Numerical Simulation of Magneto
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  • Securing Japan an Assessment of Japan´S Strategy for Space

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    Full Report Securing Japan An assessment of Japan´s strategy for space Report: Title: “ESPI Report 74 - Securing Japan - Full Report” Published: July 2020 ISSN: 2218-0931 (print) • 2076-6688 (online) Editor and publisher: European Space Policy Institute (ESPI) Schwarzenbergplatz 6 • 1030 Vienna • Austria Phone: +43 1 718 11 18 -0 E-Mail: [email protected] Website: www.espi.or.at Rights reserved - No part of this report may be reproduced or transmitted in any form or for any purpose without permission from ESPI. Citations and extracts to be published by other means are subject to mentioning “ESPI Report 74 - Securing Japan - Full Report, July 2020. All rights reserved” and sample transmission to ESPI before publishing. ESPI is not responsible for any losses, injury or damage caused to any person or property (including under contract, by negligence, product liability or otherwise) whether they may be direct or indirect, special, incidental or consequential, resulting from the information contained in this publication. Design: copylot.at Cover page picture credit: European Space Agency (ESA) TABLE OF CONTENT 1 INTRODUCTION ............................................................................................................................. 1 1.1 Background and rationales ............................................................................................................. 1 1.2 Objectives of the Study ................................................................................................................... 2 1.3 Methodology