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52. Research and development of floating platform bus technology

Author

Mita, Makoto and Fukusima, Yosuke

Abstract

第17回宇宙科学シンポジウム (2017年1月5日-6日. 宇宙航空研究開発機構宇宙科学研究所(JAXA)(ISAS)相模原キャンパス), 相模原市, 神奈川県, 17th Space Science Symposium (January 5-6, 2017. Institute of Space and Astronautical Science, Japan Aerospace Exploration Agency(JAXA)(ISAS)Sagamihara Campus), Sagamihara, Kanagawa Japan, 資料番号: SA6000060216, レポート番号: P-175

Published
2017

53. An Experimental Inertial Platform for ISAS sounding Rocket PI components

Author

Fukushima, Yosuke and Mita, Makoto

Abstract

大気球シンポジウム 平成28年度（2016年11月1-2日. 宇宙航空研究開発機構宇宙科学研究所 (JAXA)(ISAS)）, 相模原市, 神奈川県, Balloon Symposium 2016 (November 1-2, 2016. Institute of Space and Astronautical Science, Japan Aerospace Exploration Agency (JAXA)(ISAS)), Sagamihara, Kanagawa Japan, 資料番号: SA6000057018, レポート番号: isas16-sbs-018

Published
2016

55. In-Flight Performance of Ultra-lightweight X-band Deep-space Telecommunication System for PROCYON Mission

Author

Tomiki, Atsushi, Kobayashi, Yuta, Kawasaki, Shigeo, Kojima, Kaname, Shinke, Takahiro, Mochizuki, Tomoya, Aoki, Masaru, Haga, Toshiyuki, Okuno, Syuichi, Ishikawa, Masazumi, Kanda, Yasuaki, Oomori, Yoshitomo, Kitajima, Kuniyoshi, Nonomura, Taku, Mita, Makoto, Ito, Takahiro, Ito, Daichi, Kobayashi, Daisuke, Fukushima, Yosuke, Takeuchi, Hiroshi, Fujisawa, Kenta, Funase, Ryu, and Kawakatsu, Yasuhiro

Abstract

第16回宇宙科学シンポジウム (2016年1月6日-7日. 宇宙航空研究開発機構宇宙科学研究所(JAXA)(ISAS)相模原キャンパス), 相模原市, 神奈川県, 16th Space Science Symposium (January 6-7, 2016. Institute of Space and Astronautical Science, Japan Aerospace Exploration Agency(JAXA)(ISAS)Sagamihara Campus), Sagamihara, Kanagawa Japan, 著者人数: 23名, 資料番号: SA6000046055, レポート番号: P-056

Published
2016

56. Development of a small horizon sensor for sounding rockets

Author

Mita, Makoto and Fukushima, Yosuke

Abstract

第16回宇宙科学シンポジウム (2016年1月6日-7日. 宇宙航空研究開発機構宇宙科学研究所(JAXA)(ISAS)相模原キャンパス), 相模原市, 神奈川県, 16th Space Science Symposium (January 6-7, 2016. Institute of Space and Astronautical Science, Japan Aerospace Exploration Agency(JAXA)(ISAS)Sagamihara Campus), Sagamihara, Kanagawa Japan, 資料番号: SA6000046216, レポート番号: P-217

Published
2016

57. Development of Flash LIDAR device

Author

Mizuno, Takahide, Ikeda, Hirokazu, Kawahara, Kousuke, Mita, Makoto, and Kataoka, Jun

Abstract

第16回宇宙科学シンポジウム (2016年1月6日-7日. 宇宙航空研究開発機構宇宙科学研究所(JAXA)(ISAS)相模原キャンパス), 相模原市, 神奈川県, 16th Space Science Symposium (January 6-7, 2016. Institute of Space and Astronautical Science, Japan Aerospace Exploration Agency(JAXA)(ISAS)Sagamihara Campus), Sagamihara, Kanagawa Japan, 資料番号: SA6000046144, レポート番号: P-145

Published
2016

58. Developement of high power transmitter and power supplys

Author

Watanabe, Hiromi, Saito, Hirobumi, Tomiki, Atsushi, Mita, Makoto, Tomoda, Takahisa, and Kaneko, Tomoki

Abstract

第16回宇宙科学シンポジウム (2016年1月6日-7日. 宇宙航空研究開発機構宇宙科学研究所(JAXA)(ISAS)相模原キャンパス), 相模原市, 神奈川県, 16th Space Science Symposium (January 6-7, 2016. Institute of Space and Astronautical Science, Japan Aerospace Exploration Agency(JAXA)(ISAS)Sagamihara Campus), Sagamihara, Kanagawa Japan, 資料番号: SA6000046191, レポート番号: P-192

Published
2016

59. Activity of 'Research on innovative technology for satellite bus systems' RG

Author

Fukuda, Seisuke, Sakai, Shinichiro, Mita, Makoto, Ozaki, Masanobu, Tomiki, Atsushi, Matsuzaki, Keiichi, Kukita, Akio, Nakatsuka, Junichi, Sawai, Shujiro, Sato, Eiichi, Tobe, Hirobumi, Hori, Keiichi, and Katsumi, Toshiyuki

Abstract

第16回宇宙科学シンポジウム (2016年1月6日-7日. 宇宙航空研究開発機構宇宙科学研究所(JAXA)(ISAS)相模原キャンパス), 相模原市, 神奈川県, 16th Space Science Symposium (January 6-7, 2016. Institute of Space and Astronautical Science, Japan Aerospace Exploration Agency(JAXA)(ISAS)Sagamihara Campus), Sagamihara, Kanagawa Japan, 著者人数: 13名, 資料番号: SA6000046218, レポート番号: P-219

Published
2016

64. Spatial Light Phase Modulator with Bidirectional Tilt-Piston Micromirror Array - Part I: Principle and Design

Author

Hirade, Ryuichi, Yamashita, Shinji, Mita, Makoto, Fujita, Hiroyuki, Yamamoto, Tsuyoshi, Kawai, Masaaki, and Yano, Mitsuhiro

Subjects
Microelectromechanical systems, Materials science, business.industry, Mechanical Engineering, Optical communication, Silicon on insulator, law.invention, Piston, Optical modulator, Optics, law, Wafer, Electrical and Electronic Engineering, business, Phase modulation, Voltage
Abstract

Accepted: 2010-10-19, 資料番号: SA1002736000

Published
2011

65. A silicon micromachined f-thetha microlens scanner array by double-deck device design technique

Author

Kwon, Ho Nam, Lee, Jong-Hyun, Takahashi, Kazuhiro, Mita, Makoto, Saruta, Kunihiko, Fujita, Hiroyuki, and Toshiyoshi, Hiroshi

Subjects
Microlens, Scanner, Materials science, business.industry, Silicon on insulator, Atomic and Molecular Physics, and Optics, law.invention, Lens (optics), Surface micromachining, Optics, law, Etching (microfabrication), Wafer, Electrical and Electronic Engineering, Reactive-ion etching, business
Abstract

In this paper, we report an array of f- thetas microlens optical scanners developed for 3-D optical cross connect (OXC) system using the bulk-silicon micromachining technique. An electrostatic XY-stage mechanism for the 2-D lens scanner was designed to have a small footprint (2 mmtimes2 mm), compared with an integrated silicon lens (diameter 1 mm) due to the newly developed double-deck actuator design; all the mechanical parts (suspensions and frames) were made in the substrate layer of a silicon-on-insulator (SOI) wafer, and the electrostatic actuation mechanism (electrodes and electrical interconnection) was made in the SOI layer. A silicon lens was integrated on top of the XY-stage by transferring the spherical profile of a thermal-reflow photoresist pattern into the SOI layer by reactive-ion etching. The XY lens scanner was found to operate at lateral displacement of 19 mum in the X-directions and 23 mum in the Y-directions at drive voltages of 110 and 60 V, respectively. For an optical assembly of the OXC, we used additional lenses in a telescope formation to double the beam angle that was steered by the f- thetas microlens scanner by which the lens displacement could be designed to be smaller by a factor of 1/2

Published
2007

66. Lightweight X-band On-board Deep Space Telecommunication Systems for 50kg-class Ultra Small Deep Space Explorer: 'PROCYON'

Author

Kobayashi, Yuta, Tomiki, Atsushi, Kawasaki, Shigeo, Kojima, Kaname, Shinke, Takahiro, Aoki, Masaru, Tsuchiya, Shinjiro, Haga, Toshiyuki, Okuno, Shuichi, Ishikawa, Masazumi, Kanda, Yasuaki, Ohmori, Yoshitomo, Kitajima, Kunimi, Nonomura, Taku, Mita, Makoto, Ito, Taichi, Kobayashi, Daisuke, Fukushima, Yosuke, Funase, Ryu, and Kawakatsu, Yasuhiro

Abstract

第15回宇宙科学シンポジウム (2015年1月6日-7日. 宇宙航空研究開発機構宇宙科学研究所(JAXA)(ISAS)相模原キャンパス), 相模原市, 神奈川県, 15th Space Science Symposium (January 6-7, 2015. Institute of Space and Astronautical Science, Japan Aerospace Exploration Agency(JAXA)(ISAS)Sagamihara Campus), Sagamihara, Kanagawa Japan, 著者人数: 20名, 資料番号: SA6000034252, レポート番号: P-253

Published
2015

67. Development of MEMS actuators and sensors for space applications

Author

Mita, Makoto

Abstract

第15回宇宙科学シンポジウム (2015年1月6日-7日. 宇宙航空研究開発機構宇宙科学研究所(JAXA)(ISAS)相模原キャンパス), 相模原市, 神奈川県, 15th Space Science Symposium (January 6-7, 2015. Institute of Space and Astronautical Science, Japan Aerospace Exploration Agency(JAXA)(ISAS)Sagamihara Campus), Sagamihara, Kanagawa Japan, 資料番号: SA6000034289, レポート番号: P-290

Published
2015

68. Development of ROIC for Flash LIDAR

Author

Mizuno, Takahide, Ikeda, Hirokazu, Kawahara, Kousuke, and Mita, Makoto

Abstract

第15回宇宙科学シンポジウム (2015年1月6日-7日. 宇宙航空研究開発機構宇宙科学研究所(JAXA)(ISAS)相模原キャンパス), 相模原市, 神奈川県, 15th Space Science Symposium (January 6-7, 2015. Institute of Space and Astronautical Science, Japan Aerospace Exploration Agency(JAXA)(ISAS)Sagamihara Campus), Sagamihara, Kanagawa Japan, 資料番号: SA6000034186, レポート番号: P-187

Published
2015

69. Development of mono-material far-infrared filter with MEMS technolgy

Author

Yamamoto, Keita, Wada, Takehiko, Mita, Makoto, and Miyachi, Akihira

Abstract

第15回宇宙科学シンポジウム (2015年1月6日-7日. 宇宙航空研究開発機構宇宙科学研究所(JAXA)(ISAS)相模原キャンパス), 相模原市, 神奈川県, 15th Space Science Symposium (January 6-7, 2015. Institute of Space and Astronautical Science, Japan Aerospace Exploration Agency(JAXA)(ISAS)Sagamihara Campus), Sagamihara, Kanagawa Japan, 資料番号: SA6000034105, レポート番号: P-105

Published
2015

71. Performance of the initial operation of the power source system of INDEX (Reimei)

Author

Tanaka, Koji, Mita, Makoto, Okuizumi, Nobukatsu, Sone, Yoshitsugu, and Saito, Hirobumi

Subjects
宇宙機給電, リフレクタ, リチウムイオン電池, Earth observation, 太陽電池パネル, 小型科学衛星, multi-junction solar cell, solar cell panel, 地球観測, Japanese space program, spacecraft power supply, small scientific satellite, 日本の宇宙機, 多接合太陽電池, Japanese spacecraft, れいめい, エネルギー密度, lithium ion battery, energy density, 日本の宇宙計画, INDEX, reflector
Abstract

小型科学衛星INDEX(INnovative technology Demonstration EXperiment)(れいめい)は2005年8月に打ち上げられ、運用が開始された。太陽電池パドル展開後、所望の発生電力が得られ、また、バッテリーの充電回路、過電圧制御回路など電源制御系が仕様通り機能していることが確認された。, 資料番号: AA0063353056

Published
2006

72. An overview and initial in-orbit status of INDEX satellite

Author

Saito, Hirobumi, Mizuno, Takahide, Fukuda, Seisuke, Sakai, Shinichiro, Fukushima, Yosuke, Tanaka, Koji, Ikenaga, Toshinori, Okuizumi, Nobukatsu, Asamura, Kazushi, and Mita, Makoto

Subjects
小型衛星技術, 小型科学衛星, 衛星姿勢制御, aurora, 発光, satellite operation, Japanese space program, multispectral photography, small scientific satellite, 日本の宇宙機, 衛星運用, light emission, オーロラ, Japanese spacecraft, piggyback system, small satellite technology, satellite attitude control, 日本の宇宙計画, ピギーバックシステム, 多重スペクトル写真法
Abstract

This paper describes the initial on-orbit results of the small scientific satellite 'INDEX' (INnovative technology Demonstration EXperiment; REIMEI) for aurora observation and demonstration of advanced satellite technologies. REIMEI is a small satellite with 72 kg mass, and is provided with three-axis attitude control capabilities for aurora observation. REIMEI was launched into a nearly sun synchronous polar orbit on August 23rd, 2005 (UT) from Baikonur, Kazakstan by Dnepr rocket. REIMEI satellite functions work satisfactorily in the orbit. The first imaging observations of aurora were successfully performed above the southern polar region in September 16th, 2005., 資料番号: AA0063353006

Published
2006

74. Study of 2D scanning LIDAR system for deep space explorer

Author

Takahara, Takuya, Hamada, Yusuke, Mita, Makoto, Sakanoi, Takeshi, and Mizuno, Takahide

Subjects
microsatellite, sample return mission, 衛星搭載装置, 測距, Hayabusa, satellite-borne instrument, サンプルリターンミッション, はやぶさ, MEMS, 光レーダ, optical radar, calibrating, YAGレーザ, 超小型衛星, 校正, MEMSミラー, rangefinding, microelectromechanical system, ライダ, YAG laser, lidar, マイクロシャッターアレイ, micro shutter array, MEMS mirror
Abstract

Reentry scientific activities for planet and Asteroid are deployed in the world such as 'HAYABUSA' (Asteroid sample and return spacecraft, May 2003 launched), landing observation and sample return are desired as well as fly-by observation. LIDAR is mainly utilized for navigation sensor in fly-by or landing sequence. Scientific observations and landing navigators require 2-D scanning for more efficient mapping. This paper intended to study feasibility and development of 2-D scanning LIDAR with MEMS technology for deep space explorer., 資料番号: AA0049122135

Published
2005

75. Development status of high functionality small scientific satellite INDEX

Author

Saito, Hirobumi, Mizuno, Takahide, Fukuda, Seisuke, Sakai, Shinichiro, Fukushima, Yosuke, Higuchi, Ken, Okuizumi, Nobukatsu, Tanaka, Koji, Sone, Yoshitsugu, and Mita, Makoto

Subjects
majority operation, attitude control, onboard data processing, star tracker, 機上データ処理, 電源, 小型科学衛星, 衛星通信, 姿勢制御, electric power supply, リチウム電池, 統合化制御装置, 構造設計, satellite communication, thermal louver, small scientific satellite, structural design, サーマルルーバ, 多数決演算, スタートラッカ, integrated controller unit, INDEX, lithium battery
Abstract

INDEX(INnovative-technology Demonstration EXperiment)衛星は、小型3軸科学衛星のための先進的衛星技術の開発/実証を目的とした小型衛星である。また同時に、オーロラの光学カメラと粒子の同時観測による微細構造の解明を行う、という理学的目的を有している。軌道は高度600〜650kmの太陽同期軌道を予定しており、重量は約70kgである。INDEXの開発は、インハウス的なアプローチを積極的に取り入れて行われていることが特色である。以下、各サブシステムの概要と進捗状況を報告する。, 資料番号: AA0049122170

Published
2005

76. Consideration for loading a small hard disk drive on satellites

Author

Fukuda, Seisuke, Saito, Hirobumi, Mita, Makoto, and Sakai, Tomohiko

Subjects
磁気ディスク, 信頼性, reliability, Earth orbital environment, radiation tolerance, 衛星搭載装置, ハードディスクドライブ, 線量, satellite-borne instrument, satellite-borne HDD, 地球軌道環境, 不良動作, magnetic disk, gamma ray, radiation dosage, hard disk drive, 衛星搭載HDD, 放射線耐性, ガンマ線, malfunction
Abstract

資料番号: AA0049122128

Published
2005

77. Development of the lithium-ion secondary battery based on pouch type cells for piggyback satellite 'INDEX'

Author

Uno, Masatoshi, Sone, Yoshitsugu, Tanaka, Koji, Mita, Makoto, Saito, Hirobumi, and Tajima, Michio

Subjects
リチウムイオン電池, 耐放射線性, ラミネート, lithium-ion secondary battery, vacuum endurance test, space technology experiment, リチウムイオン2次電池, 環境耐性, 小型科学衛星, charge/discharge cycle test, environmental tolerance, small scientific satellite, INDEX satellite, 放射線耐性, laminate, 耐減圧環境試験, radiation hardening, ピギーバックシステム, 真空試験, radiation tolerance, aerospace environment, 宇宙技術実験, INDEX衛星, 航空宇宙環境, vacuum test, piggyback system, ピギーバック衛星, piggyback satellite, 充放電サイクル試験, lithium ion battery
Abstract

Japan Aerospace Exploration Agency (JAXA) developed piggyback satellite named INDEX. We applied lithium-ion secondary battery based on pouch cells for the satellite. The cell is designed using manganese oxide for the positive electrode and graphite carbon for the negative. The electrolyte for the lithium-ion cell is dissolved by organic solvent. Due to this configuration of the cell, the cell expands under the vacuum conditions. Since the expansion increases the DC impedance of the cell, we observed the degradation of the performance under vacuum conditions. In order to prepare the battery which is tolerant against the vacuum environment, the pouch cells were potted with resin and reinforced by the aluminum housing. More than 3,300 cycles of the charge/discharge performance was confirmed. We also tested the tolerance against the radiation using bare cells, and observed no degradation of capacity. Through these experiments, we confirmed the appropriate performance of the lithium-ion pouch cells for the operations of INDEX., 資料番号: AA0049054023, レポート番号: JAXA-SP-05-008

Published
2005

78. 50kg級超小型深宇宙探査技術実証機PROCYONの概要と開発状況

Author

船瀬, 龍, 川勝, 康弘, 福島, 洋介, 冨木, 淳史, 小林, 雄太, 中塚, 潤一, 三田, 信, 小林, 大輔, 野々村, 拓, 小泉, 宏之, 木村, 真一, 戸谷, 剛, 宮村, 典秀, 宮崎, 康行, 荒木, 友太, 亀田, 真吾, 田口, 真, 滝澤, 潤一, 細沼, 貴之, 濱口, 竜平, 五十里, 哲, 米原, 三揮, 岡田, 空馬, 尾崎, 直哉, 中谷, 俊洋, 遊馬, 貴之, 中島, 晋太郎, 古本, 拓朗, 山岸, 雄輝, 中須賀, 真一, Funase, Ryu, Kawakatsu, Yasuhiro, Fukushima, Yosuke, Tomiki, Atsushi, Kobayashi, Yuta, Nakatsuka, Junichi, Mita, Makoto, Kobayashi, Daisuke, Nonomura, Taku, Koizumi, Hiroyuki, Kimura, Shinichi, Totani, Tsuyoshi, Miyamura, Norihide, Miyazaki, Yasuyuki, Kameda, Shingo, Taguchi, Makoto, Takisawa, Junichi, Hosonuma, T., Ikari, Satoshi, Okada, Kuma, Ozaki, Naoya, Nakatani, Toshihiro, Asoma, Takayuki, Nakajima, Shintaro, Furumoto, Takuro, Yamagishi, Yuki, 船瀬, 龍, 川勝, 康弘, 福島, 洋介, 冨木, 淳史, 小林, 雄太, 中塚, 潤一, 三田, 信, 小林, 大輔, 野々村, 拓, 小泉, 宏之, 木村, 真一, 戸谷, 剛, 宮村, 典秀, 宮崎, 康行, 荒木, 友太, 亀田, 真吾, 田口, 真, 滝澤, 潤一, 細沼, 貴之, 濱口, 竜平, 五十里, 哲, 米原, 三揮, 岡田, 空馬, 尾崎, 直哉, 中谷, 俊洋, 遊馬, 貴之, 中島, 晋太郎, 古本, 拓朗, 山岸, 雄輝, 中須賀, 真一, Funase, Ryu, Kawakatsu, Yasuhiro, Fukushima, Yosuke, Tomiki, Atsushi, Kobayashi, Yuta, Nakatsuka, Junichi, Mita, Makoto, Kobayashi, Daisuke, Nonomura, Taku, Koizumi, Hiroyuki, Kimura, Shinichi, Totani, Tsuyoshi, Miyamura, Norihide, Miyazaki, Yasuyuki, Kameda, Shingo, Taguchi, Makoto, Takisawa, Junichi, Hosonuma, T., Ikari, Satoshi, Okada, Kuma, Ozaki, Naoya, Nakatani, Toshihiro, Asoma, Takayuki, Nakajima, Shintaro, Furumoto, Takuro, and Yamagishi, Yuki

Abstract

会議情報: 第14回宇宙科学シンポジウム (2014年1月9日-10日. 宇宙航空研究開発機構宇宙科学研究所(JAXA)(ISAS)相模原キャンパス), 相模原市, 神奈川県, 著者人数: 17名, Meeting Information: 14ｔh Space Science Symposium (January 9-10, 2014. Institute of Space and Astronautical Science, Japan Aerospace Exploration Agency(JAXA)(ISAS)Sagamihara Campus), Sagamihara, Kanagawa Japan

Published
2016

79. Microelectromechanical Digital-to-Analog Converters of Displacement for Step Motion Actuators

Author

Toshiyoshi, Hiroshi, Kobayashi, Dai, Mita, Makoto, Hashiguchi, Gen, Fujita, Hiroyuki, Endo, Junji, and Wada, Yasuo

Subjects
Electromechanical devices -- Design and construction, Digital-to-analog converters -- Research, Engineering and manufacturing industries, Science and technology
Abstract

This paper presents a novel micromechanism for precise positioning by using an N-bit digital code. The mechanism is an N-stage network of connected suspensions, in which an electrostatic actuator is attached to the longer suspensions of compliance 2C, and N of such unit structures are connected side by side with the shorter suspensions of compliance C. Each actuator is an electrostatic shuttle moving back and forth between the driving electrodes, and is operated by the corresponding digit of the input code. The N-bits of local displacement accumulate in the suspension network to synthesize an analog output, which is proportional to the analog value coded with the N-bit input. The output displacement is independent of the fluctuation of the driving voltage since the traveling distance of the shuttle is clipped by mechanical stoppers. We call the mechanism a microelectromechanical digital-to-analog converter (MEMDAC) since the function is equivalent to the electrical digital-to-analog converter known as the R-2R resistor network. Three different types of MEMDAC's are compared. Preliminary results of a silicon micromachined 4-bit MEMDAC successfully showed a total stroke of 5.8 [micro]m with a step of 0.38 [micro]m. The positioning resolution can be made finer by simply increasing the number of chained units. [477] Index Terms--Digital-analog conversion, displacement control, MEMS, microactuators.

Published
2000

80. 50kg-class Deep Space Exploration Technology Demonstration Micro-spacecraft PROCYON

Author

Funase, Ryu, Koizumi, Hiroyuki, Nakasuka, Shinichi, Kawakatsu, Yasuhiro, Fukushima, Yosuke, Tomiki, Atsushi, Kobayashi, Yuta, Nakatsuka, Junichi, Mita, Makoto, Kobayashi, Daisuke, and Nonomura, Taku

Abstract

University of Tokyo and Japan Aerospace Exploration Agency (JAXA) are developing a 50kg-class microspacecraft named “PROCYON” for deep space exploration. PROCYON will conduct two missions: 1) demonstration of micro-spacecraft bus system for deep space exploration, and 2) demonstration of asteroid close flyby observation. In order to develop the spacecraft with very low cost (less than a few million dollars), most of the bus system is based on that of Earth-orbiting micro satellite, excluding the communication system and propulsion system which are newly developed for the deep space mission. PROCYON is scheduled to be launched at the end of 2014 together with Japanese second asteroid sample return spacecraft Hayabusa-2. The success of PROCYON will demonstrate that a small-scale spacecraft for deep space exploration can be built with very low cost, which will enable more frequent and challenging deep space exploration.

Published
2014

81. 次世代高性能ワイヤレス化衛星を想定した宇宙エレクトロニクスによる ナノRF技術の提案

Author

Kawasaki, Shigeo, Mita, Makoto, Wada, Takehiko, Yamasaki, Noriko, and Yoshida, Satoshi

Abstract

第14回宇宙科学シンポジウム (2014年1月9日-10日. 宇宙航空研究開発機構宇宙科学研究所(JAXA)(ISAS)相模原キャンパス), 相模原市, 神奈川県, 14ｔh Space Science Symposium (January 9-10, 2014. Institute of Space and Astronautical Science, Japan Aerospace Exploration Agency(JAXA)(ISAS)Sagamihara Campus), Sagamihara, Kanagawa Japan, 資料番号: SA6000058025, レポート番号: S2-017

Published
2014

82. 50kg級超小型深宇宙探査機PROCYONにおける軽量X帯搭載深宇宙通信システムの開発

Author

Kobayashi, Yuta, Tomiki, Atsushi, Kawasaki, Shigeo, Kojima, Kaname, Shinke, Takahiro, Aoki, Masaru, Tsuchiya, Shinjiro, Haga, Toshiyuki, Okuno, Shuichi, Ishikawa, Masazumi, Kanda, Yasuaki, Ohmori, Yoshitomo, Nonomura, Taku, Mita, Makoto, Kobayashi, Daisuke, Fukushima, Yosuke, Funase, Ryu, and Kawakatsu, Yasuhiro

Abstract

第14回宇宙科学シンポジウム (2014年1月9日-10日. 宇宙航空研究開発機構宇宙科学研究所(JAXA)(ISAS)相模原キャンパス), 相模原市, 神奈川県, 14ｔh Space Science Symposium (January 9-10, 2014. Institute of Space and Astronautical Science, Japan Aerospace Exploration Agency(JAXA)(ISAS)Sagamihara Campus), Sagamihara, Kanagawa Japan, 著者人数: 18名, 資料番号: SA6000058157, レポート番号: P2-125

Published
2014

83. MEMS技術を用いた赤外線・テラヘルツ単一材料光学干渉フィルターの研究

Author

Yamamoto, Keita, Wada, Takehiko, and Mita, Makoto

Abstract

第14回宇宙科学シンポジウム (2014年1月9日-10日. 宇宙航空研究開発機構宇宙科学研究所(JAXA)(ISAS)相模原キャンパス), 相模原市, 神奈川県, 14th Space Science Symposium (January 9-10, 2014. Institute of Space and Astronautical Science, Japan Aerospace Exploration Agency(JAXA)(ISAS)Sagamihara Campus), Sagamihara, Kanagawa Japan, 資料番号: SA6000058283, レポート番号: P2-251

Published
2014

84. 50kg級超小型深宇宙探査技術実証機PROCYONの概要と開発状況

Author

Funase, Ryu, Kawakatsu, Yasuhiro, Fukushima, Yosuke, Tomiki, Atsushi, Kobayashi, Yuta, Nakatsuka, Junichi, Mita, Makoto, Kobayashi, Daisuke, Nonomura, Taku, Koizumi, Hiroyuki, Kimura, Shinichi, Totani, Tsuyoshi, Miyamura, Norihide, Miyazaki, Yasuyuki, Kameda, Shingo, Taguchi, Makoto, Takisawa, Junichi, Hosonuma, T., Ikari, Satoshi, Okada, Kuma, Ozaki, Naoya, Nakatani, Toshihiro, Asoma, Takayuki, Nakajima, Shintaro, Furumoto, Takuro, and Yamagishi, Yuki

Abstract

第14回宇宙科学シンポジウム (2014年1月9日-10日. 宇宙航空研究開発機構宇宙科学研究所(JAXA)(ISAS)相模原キャンパス), 相模原市, 神奈川県, 14ｔh Space Science Symposium (January 9-10, 2014. Institute of Space and Astronautical Science, Japan Aerospace Exploration Agency(JAXA)(ISAS)Sagamihara Campus), Sagamihara, Kanagawa Japan, 著者人数: 17名, 資料番号: SA6000058012, レポート番号: S2-004

Published
2014

86. Design of corrugated-horn-coupled MKID focal plane for CMB B-mode polarization

Author

Sekimoto, Yutaro, additional, Sekiguchi, Shigeyuki, additional, Shu, Shibo, additional, Sekine, Masakazu, additional, Nitta, Tom, additional, Naruse, Masato, additional, Dominjon, Agnes, additional, Hasebe, Takashi, additional, Shan, Wenlei, additional, Noguchi, Takashi, additional, Miyachi, Akihira, additional, Mita, Makoto, additional, and Kawasaki, Shigeo, additional

Published
2016
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88. 小型高機能科学衛星INDEXの開発と現状

Author

Saito, Hirobumi, Mizuno, Takahide, Fukuda, Seisuke, Sakai, Shinichiro, Fukushima, Yosuke, Higuchi, Ken, Okuizumi, Nobukatsu, Tanaka, Koji, Sone, Yoshitsugu, Mita, Makoto, 斎藤 宏文, 水野 貴秀, 福田 盛介, 坂井 真一郎, 福島 洋介, 樋口 健, 奥泉 信克, 田中 孝治, 曽根 理嗣, 三田 信, Saito, Hirobumi, Mizuno, Takahide, Fukuda, Seisuke, Sakai, Shinichiro, Fukushima, Yosuke, Higuchi, Ken, Okuizumi, Nobukatsu, Tanaka, Koji, Sone, Yoshitsugu, Mita, Makoto, 斎藤 宏文, 水野 貴秀, 福田 盛介, 坂井 真一郎, 福島 洋介, 樋口 健, 奥泉 信克, 田中 孝治, 曽根 理嗣, and 三田 信

Abstract

INDEX(INnovative-technology Demonstration EXperiment)衛星は、小型3軸科学衛星のための先進的衛星技術の開発/実証を目的とした小型衛星である。また同時に、オーロラの光学カメラと粒子の同時観測による微細構造の解明を行う、という理学的目的を有している。軌道は高度600〜650kmの太陽同期軌道を予定しており、重量は約70kgである。INDEXの開発は、インハウス的なアプローチを積極的に取り入れて行われていることが特色である。以下、各サブシステムの概要と進捗状況を報告する。

Published
2015

89. An Equivalent Circuit Model for Vertical Comb Drive MEMS Optical Scanner Controlled by Pulse Width Modulation

Author

丸山, 智史, 中田, 宗樹, 三田, 信, 高橋, 巧也, 藤田, 博之, 年吉, 洋, Maruyama, Satoshi, Nakada, Muneki, Mita, Makoto, Takahashi, Takuya, Fujita, Hiroyuki, Toshiyoshi, Hiroshi, 丸山, 智史, 中田, 宗樹, 三田, 信, 高橋, 巧也, 藤田, 博之, 年吉, 洋, Maruyama, Satoshi, Nakada, Muneki, Mita, Makoto, Takahashi, Takuya, Fujita, Hiroyuki, and Toshiyoshi, Hiroshi

Published
2015

90. Development Status of Hayabusa-2 LIDAR

Author

Senshu, Hiroki, Yamada, Ryuhei, Kobayashi, Masanori, Namiki, Noriyuki, Mizuno, Takahide, Mita, Makoto, Kawahara, Kousuke, and Kunimori, Hiroo

Abstract

第46回月・惑星シンポジウム (2013年8月5日-7日. 宇宙航空研究開発機構宇宙科学研究所), 相模原市, 神奈川県, 46th ISAS Lunar and Planetary Symposium (August 5-7, 2013. Institute of Space and Astronautical Science, Japan Aerospace Exploration Agency (JAXA)(ISAS)), Sagamihara, Kanagawa Japan, 形態: カラー図版あり, 形態: CD-ROM1枚, 資料番号: SA6000015039

Published
2013

91. 宇宙通信とセンサーネットワークのための混成半導体集積回路

Author

Hirahara, Daichi, Mita, Makoto, and Kawasaki, Shigeo

Abstract

第13回宇宙科学シンポジウム (2013年1月8日-9日. 宇宙航空研究開発機構宇宙科学研究所(JAXA)(ISAS)相模原キャンパス), 相模原市, 神奈川県, 13th Space Science Symposium (January 8-9, 2013. Institute of Space and Astronautical Science, Japan Aerospace Exploration Agency(JAXA)(ISAS)Sagamihara Campus), Sagamihara, Kanagawa Japan, 資料番号: SA6000063321, レポート番号: P5-059

Published
2013

92. SPICAコロナグラフ装置（SCI）

Author

Abe, Lyu, Guyon, Olivier, Enya, Keigo, Kaneda, Hidehiro, Kotani, Takayuki, Haze, Kanae, Oyabu, Shinki, Ishihara, Daisuke, Nakagawa, Takao, Matsuhara, Hideo, Kataza, Hirokazu, Kawada, Mitsunobu, Wada, Takehiko, Tsumura, Koji, Mita, Makoto, Komatsu, Keiji, Uchida, Hideki, Mitani, Shinji, Sakai, Shinichiro, Sarugaku, Yuki, Arimatsu, Ko, Sorahana, Satoko, Tao, Chihiro, Miyata, Takashi, Asano, Kentaroh, Nakamura, Tomohiko, Kamizuka, Takafumi, Uchiyama, Mizuho, Matsuo, Taro, Ikoma, Masahiro, Honda, Mitsuhiko, Inoue, Akio K., Itoh, Yoichi, Ida, Shigeru, Nagasawa, Makiko, Takami, Michihiro, Fukagawa, Misato, Shibai, Hiroshi, Baba, Naoshi, Murakami, Naoshi, Okamoto, Yoshiko, Yamashita, Takuya, Narita, Norio, Tamura, Motohide, Nishikawa, Jun, Hayano, Yutaka, Oya, Shin, Kokubo, Eiichiro, Izumiura, Hideyuki, Sasaki, Sho, Oseki, Shinji, Yamagishi, Mitsuyoshi, Yasuda, Akiko, Yamada, Rika, Fujishiro, Naofumi, Ikeda, Yuji, Kobayashi, Hitomi, and Yamamuro, Tomoyasu

Abstract

第13回宇宙科学シンポジウム (2013年1月8日-9日. 宇宙航空研究開発機構宇宙科学研究所(JAXA)(ISAS)相模原キャンパス), 相模原市, 神奈川県, 13th Space Science Symposium (January 8-9, 2013. Institute of Space and Astronautical Science, Japan Aerospace Exploration Agency(JAXA)(ISAS)Sagamihara Campus), Sagamihara, Kanagawa Japan, 著者人数: 59名, 資料番号: SA6000063076, レポート番号: P2-049

Published
2013

94. 宇宙通信とセンサーネットワークのための混成半導体集積回路の初期研究

Author

Hirahara, Daichi, Mita, Makoto, and Kawasaki, Shigeo

Abstract

第12回宇宙科学シンポジウム (2012年1月5日-6日. 宇宙航空研究開発機構宇宙科学研究所(JAXA)(ISAS)相模原キャンパス), 相模原市, 神奈川県, 12th Space Science Symposium (January 5-6, 2012. Institute of Space and Astronautical Science, Japan Aerospace Exploration Agency(JAXA)(ISAS)Sagamihara Campus), Sagamihara, Kanagawa Japan, 資料番号: SA6000064282, レポート番号: P5-003

Published
2012

95. サブ波長構造を利用した単一材料による赤外線多層干渉フィルター

Author

Makitsubo, Hironobu, Wada, Takehiko, Mita, Makoto, and Suzuki, Toyoaki

Abstract

第12回宇宙科学シンポジウム (2012年1月5日-6日. 宇宙航空研究開発機構宇宙科学研究所(JAXA)(ISAS)相模原キャンパス), 相模原市, 神奈川県, 12th Space Science Symposium (January 5-6, 2012. Institute of Space and Astronautical Science, Japan Aerospace Exploration Agency(JAXA)(ISAS)Sagamihara Campus), Sagamihara, Kanagawa Japan, 資料番号: SA6000064311, レポート番号: P5-065

Published
2012

96. Single material infrared multilayer interference filter using Sub-Wavelength Structures (SWS)

Author

Makitsubo, Hironobu, Wada, Takehiko, and Mita, Makoto

Abstract

第11回宇宙科学シンポジウム (2011年1月5日-7日. 宇宙航空研究開発機構宇宙科学研究所相模原キャンパス), 相模原市, 神奈川県, 11th Space Science Symposium (January 5-7, 2011. Institute of Space and Astronautical Science, Japan Aerospace Exploration Agency), Sagamihara, Kanagawa Japan, 我々は天文衛星による高感度な赤外線観測を用いた天文学研究に向けて、高性能で冷却サイクルに強い中間・遠赤外線フィルターの開発を目指している。, 実現に向けて、一般的なMEMS技術のみを用いて作製可能な、サブ波長構造を用いた単一材料多層干渉フィルターを提案している。, 本講演では、開発の鍵となる「サブ波長構造による屈折率制御」の検証実験を行い、屈折率を制御できることを実証したので報告する。, 形態: カラー図版あり, 形態: CD-ROM1枚, Physical characteristics: Original contains color illustrations, Note: One CD-ROM, 資料番号: AA0065426261

Published
2011

97. Fabrication of Metamaterial Microwave Transmission-Line Utilizing Semiconductor Integration Technology

Author

Hirahara, Daichi, Noji, Hirofumi, Hori, Masakazu, Isono, Kosuke, Mita, Makoto, and Kawasaki, Shigeo

Abstract

第11回宇宙科学シンポジウム (2011年1月5日-7日. 宇宙航空研究開発機構宇宙科学研究所相模原キャンパス), 相模原市, 神奈川県, 11th Space Science Symposium (January 5-7, 2011. Institute of Space and Astronautical Science, Japan Aerospace Exploration Agency), Sagamihara, Kanagawa Japan, 形態: カラー図版あり, 形態: CD-ROM1枚, Physical characteristics: Original contains color illustrations, Note: One CD-ROM, 資料番号: AA0065426283

Published
2011

98. Observation of extrasolar planets by coronagraph instrument onboard next generation satellite Space Infrared Telescope for Cosmology and Astrophysics SPICA

Author

Enya, Keigo, Kotani, Takayuki, Nakagawa, Takao, Kataza, Hirokazu, Matsuhara, Hideo, Wada, Takehiko, Kawada, Mitsunobu, Mita, Makoto, Takeuchi, Shinsuke, Komatsu, Keiji, Uchida, Hideki, Fujiwara, Ken, Mitani, Shinji, and Sakai, Shinichiro

Abstract

第33回太陽系科学シンポジウム (2011年11月15-16日. 宇宙航空研究開発機構宇宙科学研究所), 相模原市, 神奈川県, 33rd Solar System Exploration Symposium (November 15-16, 2011. Institute of Space and Astronautical Science, Japan Aerospace Exploration Agency(JAXA)(ISAS)), Sagamihara, Kanagawa Japan, 形態: カラー図版あり, 形態: CD-ROM1枚, 著者人数: 41人, Physical characteristics: Original contains color illustrations, Note: One CD-ROM, Number of authors: 41, 資料番号: AA0065389015

Published
2011

99. 宇宙科学を支えるテクノロジー

Author

Fukushima, Yosuke, Mita, Makoto, and Otsuki, Masatsugu

Abstract

第11回宇宙科学シンポジウム (2011年1月5日-7日. 宇宙航空研究開発機構宇宙科学研究所相模原キャンパス), 相模原市, 神奈川県, 11th Space Science Symposium (January 5-7, 2011. Institute of Space and Astronautical Science, Japan Aerospace Exploration Agency), Sagamihara, Kanagawa Japan, 形態: カラー図版あり, 形態: CD-ROM1枚, Physical characteristics: Original contains color illustrations, Note: One CD-ROM, 資料番号: AA0065426289

Published
2011

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