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  2. 阿部 琢美

阿部 琢美

アベ タクミ  (Takumi ABE)

基本情報

所属
国立研究開発法人宇宙航空研究開発機構 宇宙科学研究所 太陽系科学研究系 准教授
総合研究大学院大学（総研大） 物理科学研究科 宇宙科学専攻 准教授
J-GLOBAL ID
200901006137313045
researchmap会員ID
1000253786
外部リンク

研究キーワード

 5

研究分野

 1

経歴

 4

学歴

 3

委員歴

 1

受賞

 1

論文

 125
  • Sorai Teraoka, Huixin Liu, Michi Nishioka, Susumu Saito, Toru Takahashi, Atsushi Kumamoto, Yuki Ashihara, Takumi Abe
    EARTH PLANETS AND SPACE 77(1) 2025年2月25日  
    The measurement of virtual height of the sporadic E layer (h'Es) is very sensitive to the type of ionosonde used and the calibration processes. The ionosondes used by the national institute of communication and technology (NICT) has changed several times in the past, resulting in large differences in h'Es before and after the change. We propose a simple method to calibrate h'Es. We used the data of ionosonde observations at four stations, i.e., Wakkanai (45.16 degrees N, 141.75 degrees E), Tokyo (35.71 degrees N, 139.49 degrees E), Yamagawa (31.20 degrees N, 130.62 degrees E), Okinawa (26.68 degrees N, 128.15 degrees E) to calibrate the latest ionosondes VIPIR2, which were installed in May 2017. We carried out the analysis by applying the double-reflection method to the original ionogram images between 2017 and 2021. By developing an automated image detecting algorithm, we were able to process a large amount of data and achieve a calibration with high accuracy. As a result, it was found that the current VIPIR2 data had an offset of 26-28 km.
  • 佐藤毅彦, 山崎敦, 今村剛, 石井信明, 中村正人, 阿部琢美
    日本惑星科学会誌 遊・星・人 33(1) 74-77 2024年3月  
  • Laila Andersson, Takumi Abe, Hassanali Akbari, Edgar Bering, John W. Bonnell, Anders Eriksson, Jean-Pierre Lebreton, Wojciech Miloch, Sylvain Ranvier
    AIAA SCITECH 2024 FORUM 2024年  
    One of the first instruments used to monitor laboratory plasmas was the Langmuir probe (LP). This instrument is still one of the key sensors in laboratory plasma investigations. With the access to space, the first sounding rockets with Langmuir Probes were flown in 1946-1947; followed with Langmuir probes on satellites from the early 1960s and on Pioneer Venus Orbiter and subsequent interplanetary probes starting in the 1970s. This paper summarizes some of the experiences of using Langmuir probes over the last 75-years in space, what issues have been encountered, and how to overcome different known effects unique to space flight measurements. This work was done through a number of workshops attended by a number of instrument team members and supported by the ISSI organisation.
  • Masatoshi Yamauchi, Johan De Keyser, George Parks, Shin ichiro Oyama, Peter Wurz, Takumi Abe, Arnaud Beth, Ioannis A. Daglis, Iannis Dandouras, Malcolm Dunlop, Pierre Henri, Nickolay Ivchenko, Esa Kallio, Harald Kucharek, Yong C.M. Liu, Ingrid Mann, Octav Marghitu, Georgios Nicolaou, Zhaojin Rong, Takeshi Sakanoi, Joachim Saur, Manabu Shimoyama, Satoshi Taguchi, Feng Tian, Takuo Tsuda, Bruce Tsurutani, Drew Turner, Thomas Ulich, Andrew Yau, Ichiro Yoshikawa
    Experimental Astronomy 54(2-3) 521-559 2022年12月  査読有り
    In the White Paper, submitted in response to the European Space Agency (ESA) Voyage 2050 Call, we present the importance of advancing our knowledge of plasma-neutral gas interactions, and of deepening our understanding of the partially ionized environments that are ubiquitous in the upper atmospheres of planets and moons, and elsewhere in space. In future space missions, the above task requires addressing the following fundamental questions: (A) How and by how much do plasma-neutral gas interactions influence the re-distribution of externally provided energy to the composing species? (B) How and by how much do plasma-neutral gas interactions contribute toward the growth of heavy complex molecules and biomolecules? Answering these questions is an absolute prerequisite for addressing the long-standing questions of atmospheric escape, the origin of biomolecules, and their role in the evolution of planets, moons, or comets, under the influence of energy sources in the form of electromagnetic and corpuscular radiation, because low-energy ion-neutral cross-sections in space cannot be reproduced quantitatively in laboratories for conditions of satisfying, particularly, (1) low-temperatures, (2) tenuous or strong gradients or layered media, and (3) in low-gravity plasma. Measurements with a minimum core instrument package (< 15 kg) can be used to perform such investigations in many different conditions and should be included in all deep-space missions. These investigations, if specific ranges of background parameters are considered, can also be pursued for Earth, Mars, and Venus.
  • 阿部琢美, 渡部重十, YAU Andrew, 北村成寿
    プラズマ・核融合学会誌 98(11) 472-476 2022年11月  
もっとみる

MISC

 55
  • 阿部 琢美
    真空ジャーナル (178) 10-14 2021年10月  
  • 田寺, 慶樹, 阿部, 琢美, 三宅, 亙
    東海大学紀要. 工学部 57(2) 49-53 2018年3月31日  
  • Masato Nakamura, Nobuaki Ishii, Takeshi Imamura, Takehiko Satoh, Takumi Abe, Chikako Hirose, Atsushi Yamazaki, Junichi Nakatsuka, Tsutomu Ichikawa, Tomoaki Toda, Hiroyuki Toyoda, Sumitaka Tachikawa, Yukio Kamata, Makoto Suzuki, Takao M. Sato, Shin Ya Murakami, Yukio Yamamoto, Naomoto Iwagami, Makoto Taguchi, Tesuya Fukuhara, Shigeto Watanabe, Yukihiro Takahashi, Munetaka Ueno, Manabu Yamada, George L. Hashimoto, Naru Hirata, Toru Kouyama, Kazunori Ogohara, Hiroki Ando, Koichiro Sugiyama, Hiroki Kashimura, Shoko Ohtsuki
    Proceedings of the International Astronautical Congress, IAC 2016年1月1日  
    Copyright © 2016 by the International Astronautical Federation (IAF). All rights reserved. Japan&#039;s Venus Climate Orbiter Akatsuki was proposed to ISAS (Institute of Space and Astronautical Science) in 2001 as an interplanetary mission. We made 5 cameras with narrow-band filters to image Venus at different wavelengths to track the cloud and minor components distribution at different heights to study the Venusian atmospheric dynamics in 3 dimension. It was launched on May 21st, 2010 and reached Venus on December 7th, 2010. With the thrust by the orbital maneuver engine, Akatsuki tried to go into the westward equatorial orbit around Venus with the 30 hours&#039; orbital period, however it failed by the malfunction of the propulsion system. Later the spacecraft has been orbiting the sun for 5 years. On December 7th, 2015 Akatsuki met Venus again after the orbit control and Akatsuki was put into the westward equatorial orbit whose apoapsis is about 0.44 million km and orbital period of 14 days. Its main target is to shed light on the mechanism of the fast atmospheric circulation of Venus. The systematic imaging sequence by Akatsuki is advantageous for detecting meteorological phenomena with various temporal and spatial scales. We have five photometric sensors as mission instruments for imaging, which are 1 m-infrared camera (IR1), 2 m-infrared camera (IR2), ultra-violet imager (UVI), long-wave infrared camera (LIR), and lightning and airglow camera (LAC). These photometers except LIR have changeable filters in the optics to image in certain wavelengths. Akatsuki&#039;s long elliptical orbit around Venus is suitable for obtaining cloud-tracked wind vectors over a wide area continuously from high altitudes. With the observation, the characterizations of the meridional circulation, mid-latitude jets, and various wave activities are anticipated. The technical issues of Venus orbit insertion in 2015 and the scientific new results will be given in this paper.
  • 阿部 琢美
    平成25年度第1次観測ロケットS-310-42号機・S-520-27号機飛翔実験報告書 SES-TD-14-004 181-183 2015年  
  • 阿部琢美
    ISASニュース (378) 2012年  
もっとみる

書籍等出版物

 2

講演・口頭発表等

 307
  • 北野谷有吾, 阿部琢美
    大気圏シンポジウム・講演集(Web) 2010年
  • 中村正人, 石井信明, 今村剛, 上野宗孝, 鈴木睦, 阿部琢美, 山崎敦, 岩上直幹, 佐藤毅彦, 田口真, 渡部重十, 福原哲哉, 大月祥子
    地球電磁気・地球惑星圏学会総会及び講演会予稿集(CD-ROM) 2010年
  • 松岡彩子, 阿部琢美, 石坂圭吾, 熊本篤志, 栗原純一, 関華奈子, 田口真, 寺田直樹, 二穴喜文, 八木谷聡, 山崎敦, 横田勝一郎, 松岡彩子
    地球電磁気・地球惑星圏学会総会及び講演会予稿集(CD−ROM) 2010年
  • 齊藤昭則, 阿部琢美, 山崎敦, 鈴木睦, 坂野井健, 藤原均, 吉川一朗, 大塚雄一, 田口真, 山本衛, 中村卓司, 菊池雅行, 江尻省, 河野英昭, 石井守, 久保田実, 星野尾一明, 坂野井和代
    第10回宇宙科学シンポジウム講演集 2010年
  • KITAMURA Naritoshi, TERADA Naoki, OGAWA Yasunobu, ABE Takumi, ONO Takayuki, NISHIMURA Yukitoshi, SHINBORI Atsuki, KUMAMOTO Atsushi
    極域科学・宙空圏・気水圏・生物・地学シンポジウム講演予稿集(CD-ROM) 2010年
  • KITAMURA Naritoshi, TERADA Naoki, OGAWA Yasunobu, ABE Takumi, ONO Takayuki, NISHIMURA Yukitoshi, SHINBORI Atsuki, KUMAMOTO Atsushi
    地球電磁気・地球惑星圏学会総会及び講演会予稿集(CD-ROM) 2010年
  • 森永隆稔, 山本真行, 栗原純一, LARSEN Miguel, 久保田賢, 大山伸一郎, 野澤悟徳, 小川泰信, 阿部琢美, 渡部重十
    地球電磁気・地球惑星圏学会総会及び講演会予稿集(CD-ROM) 2010年
  • 笠羽康正, 石坂圭吾, 熊本篤志, 鈴木朋憲, 阿部琢美, 下山学
    スペース・プラズマ研究会 2009年
  • 住野諒, 佐原宏典, 田中孝治, 佐々木進, 下山学, 阿部琢美, 山極芳樹, 神戸篤, 若槻賢, 藤井裕矩
    スペース・プラズマ研究会 2009年
  • 森本健志, 牛尾知雄, 佐藤光輝, 高橋幸弘, INAN Umran, 芳原容英, 菊池雅行, 鈴木睦, 山崎敦, 阿部琢美, 吉田和哉, 坂本祐二, 奥山圭一, 石田良平, 河崎善一郎
    大気圏シンポジウム・講演集(Web) 2009年
  • 北野谷有吾, 阿部琢美
    大気圏シンポジウム・講演集(Web) 2009年
  • 高橋幸弘, 嘉瀬浩美, 牛尾知雄, 森本健志, 佐藤光輝, INAN Umran, 芳原容英, 菊池雅行, 鈴木睦, 山崎敦, 阿部琢美, 吉田和哉, 坂本祐二, 奥山圭一, 石田良平, 河崎善一郎
    大気圏シンポジウム・講演集(Web) 2009年
  • 牛尾知雄, 鈴木睦, 佐藤光輝, 森本健志, 高橋幸弘, 芳原容英, 菊池雅行, INAN Umran, 山崎敦, 阿部琢美, 河崎善一郎
    大気圏シンポジウム・講演集(Web) 2009年
  • 鈴木睦, 山崎敦, 阿部琢美, 織田裕久
    大気圏シンポジウム・講演集(Web) 2009年
  • 佐藤光輝, 牛尾知雄, 森本健志, 高橋幸弘, INAN Umran, 芳原容英, 菊池雅行, 石田良平, 吉田和哉, 坂本祐二, 奥山圭一, 河崎善一郎, 鈴木睦, 山崎敦, 阿部琢美
    大気圏シンポジウム・講演集(Web) 2009年
  • 藤井裕矩, 藤井裕矩, 渡部武夫, 佐原宏典, 間沢朋哉, 竹原昭一郎, 山極芳樹, 大津広敬, 田中孝治, 阿部琢美, 下山学, 佐々木進, 小山孝一郎
    アストロダイナミクスシンポジウム講演後刷り集(Web) 2009年
  • 栗原純一, 栗原宜子, 岩上直幹, 鈴木朋憲, 熊本篤志, 小野高幸, 中村真帆, 石井守, 松岡彩子, 石坂圭吾, 阿部琢美, 野澤悟徳
    大気圏シンポジウム・講演集(Web) 2009年
  • 坂野井健, 山崎敦, 大塚雄一, 田口真, 阿部琢美, 武山芸英, 小淵保幸, 齊藤昭則, 江尻省, 中村卓司, 鈴木睦, 久保田実, 吉川一朗, 星野尾一明, 坂野井和代, 藤原均, 山本衛, 石井守, 陣英克, 河野英昭
    大気圏シンポジウム・講演集(Web) 2009年
  • 森永隆稔, 山本真行, 横山雄生, 栗原純一, LARSEN Miguel F, 大山伸一郎, 野澤悟徳, 小川泰信, 吉田健悟, 阿部琢美, 渡部重十, 岩上直幹
    地球電磁気・地球惑星圏学会総会及び講演会予稿集(CD−ROM) 2009年
  • 阿部琢美, 小川泰信, MOEN Joran
    地球電磁気・地球惑星圏学会総会及び講演会予稿集(CD-ROM) 2009年
  • Takumi Abe, Masato Nakamura, Nobuaki Ishii, Yoshifumi Inatani
    PROCEEDINGS OF THE 19TH ESA SYMPOSIUM ON EUROPEAN ROCKET AND BALLOON PROGRAMMES AND RELATED RESEARCH 2009年 EUROPEAN SPACE AGENCY
    Sounding rocket experiments have been successively conducted for more than 40 years in Japan. These include various scientific and engineering topics. In this paper, we present recent activities of Japanese sounding rocket experiments for the last two years (2007-2008 fiscal year) and also describe a future direction on the experiment in the mid-term range.
  • 藤井, 裕矩, 渡部, 武夫, 草谷, 大郎, 小島, 広久, 小山, 孝一郎, 佐々木, 進, 田中, 孝治, 阿部, 琢美, 下山, 学, 山極, 芳樹, Fujii, Hironori A., Watanabe, Takeo, Kusagaya, Tairo, Kojima, Hirohisa, Oyama, Koichiro, Sasaki, Susumu, Tanaka, Koji, Abe, Takumi, Shimoyama, Manabu, Yamagiwa, Yoshiki
    宇宙利用シンポジウム 第24回 平成19年度 = Space Utilization Research: Proceedings of the Twenty-fourth Space Utilization Symposium 2008年3月 宇宙航空研究開発機構宇宙科学研究本部
    Two projects are introduced in this paper to verify the performance of space tether technology. A sounding rocket will be launched in the summer of 2009 to deploy a bare electro-dynamic tape tether having a length of 300 m. The other project to verify the space tether technology is a small satellite to deploy a bare 25 km electro-dynamic tape tether, and the launch is expected in 2013 with employing a new solid motor rocket. These verifications of tether technology will lead to a large numbers of applications of space tether technology and some future projects are also introduced. 資料番号: AA0063706026
  • 栗原純一, 栗原宜子, 岩上直幹, 鈴木朋憲, 熊本篤志, 小野高幸, 中村真帆, 石井守, 松岡彩子, 石坂圭吾, 阿部琢美, 野澤悟徳
    地球電磁気・地球惑星圏学会総会及び講演会予稿集(CD-ROM) 2008年
  • 横山雄生, 山本真行, 渡部重十, 阿部琢美, 羽生宏人, 小野高幸, 大塚雄一, 齊藤昭則
    地球電磁気・地球惑星圏学会総会及び講演会予稿集(CD-ROM) 2008年
  • 齊藤昭則, 阿部琢美, 坂野井健, 大塚雄一, 田口真, 吉川一朗, 山崎敦, 鈴木睦, 中村卓司, 山本衛, 河野英昭, 石井守, 星野尾一明, 坂野井和代, 藤原均, 久保田実, 江尻省
    地球電磁気・地球惑星圏学会総会及び講演会予稿集(CD-ROM) 2008年
  • KURIHARA Junichi, OYAMA Shin‐ichiro, NOZAWA Satonori, FUJII Ryoichi, OGAWA Yasunobu, IWAGAMI Naomoto, ABE Takumi
    地球電磁気・地球惑星圏学会総会及び講演会予稿集(CD-ROM) 2008年
  • 小川泰信, 宮岡宏, 藤井良一, 野澤悟徳, 大山伸一郎, 平原聖文, 坂野井健, 阿部琢美, 小野高幸, 細川敬祐, 門倉昭, 行松彰
    地球電磁気・地球惑星圏学会総会及び講演会予稿集(CD-ROM) 2008年
  • 南部慎吾, 渡部重十, 阿部琢美, 羽生宏人, 中村正人, 小野高幸, 大塚雄一, 山本衛, 齊藤昭則, 山本真行
    地球電磁気・地球惑星圏学会総会及び講演会予稿集(CD-ROM) 2008年
  • 山本真行, 横山雄生, 渡部重十, 阿部琢美, 羽生宏人, 大塚雄一, 齊藤昭則, 山本衛, 小野高幸
    大気圏シンポジウム 2008年
  • Yoshifumi Inatani, Nobuaki Ishii, Takumi Abe, Tetsuya Yoshida
    European Space Agency, (Special Publication) ESA SP 2007年6月 ESA PUBLICATIONS DIVISION C/O ESTEC
    In the fiscal year of 2005 and 2006, Japan Aerospace Exploration Agency (JAXA) had successfully launched 10 space vehicles, which included five application satellites, three scientific observation satellites and two sounding rockets with a single stage solid motor. The Institute of Space and Astronautical Science (ISAS) has been continuously conducting space science programs using sounding rockets, scientific satellites and stratospheric balloons. This paper briefly introduces and summarizes the ISAS space activities in the two years.
  • 門畑顕博, 阿部琢美, 小山孝一郎, 岩上直幹, 栗原純一, 若林誠, 野澤悟徳, 藤井良一, 小川泰信
    大気圏シンポジウム 2007年6月
  • Satoshi Nonaka, Hiroyuki Ogawa, Yoshihiro Naruo, Nobuaki Ishii, Takumi Abe, Yoshifumi Inatani
    European Space Agency, (Special Publication) ESA SP 2007年6月 ESA PUBLICATIONS DIVISION C/O ESTEC
    A fully reusable rocket vehicle is proposed as a sounding rocket for observations of atmospheric phenomena, micro-gravity experiments and so on. Vehicle systems and ground / flight operations are designed for such science observations. For the development of the reusable rocket, a small test vehicle was built and flight-tested. This Reusable Vehicle Testing (RVT) lessons campaign provide repeated experiences of turnaround operations and vertical take-off and landing flights. In the present design of the reusable sounding rocket, the total length and maximum diameter of the vehicle is about 10m and 3m, respectively. The vehicle is propelled by the propulsion system composed of four liquid hydrogen / liquid oxygen engines. The weight of a payload carried to 120 km altitude is 100kg in the nose-fairing. The instrument for observations can be reused because of the repeated flight. The turnaround time for one flight is less than 24 hours (1 day). In the typical ballistic flight up to 120 km, the flight environments under 10(-5)G acceleration is able to be made for about 120 sec. The flight Mach number can be subsonic around the summit in the trajectory. These properties of reusable sounding rocket are expected to be useful and effective for many science missions.
  • Manabu Shimoyama, Takumi Abe, Koh Ichiro Oyama
    European Space Agency, (Special Publication) ESA SP 2007年6月 ESA PUBLICATIONS DIVISION C/O ESTEC
    Processes of energy cascade from suprathermal to thermal electrons significantly affect the thermal structure of the lower ionosphere. The Suprathermal Plasma Analyzer (SPA) was developed to measure an energy distribution of thermal and suprathermal electrons (&lt; 5 eV). The principle of this analyzer is based on the innovative combination of a second harmonic method and a channel electron multiplier. Outstanding point of this analyzer are: 1) accurate calibration of electron energy within the order of 0.01 eV, and 2) the energy resolution smaller than 0.15 eV. The SPA was installed in the sounding rocket S-310-37 and observed the electron energy distribution function at the height from 100 km to 140 km.
  • Takumi Abe, Manabu Shimoyama, Keigo Ishisaka, Toshimi Okada, Fumio Tohyama, Takao Takahashi, Kiyohumi Yumoto, Koh Ichiro Oyama
    European Space Agency, (Special Publication) ESA SP 2007年6月 ESA PUBLICATIONS DIVISION C/O ESTEC
    The sounding rocket measurements in the mid-latitude ionosphere suggest that the electron temperature occasionally increases at 100-110 km altitudes during daytime in winter. Detailed study indicates that such a temperature increase is closely related to the existence of the Sq current focus, because the temperature increase becomes significant when the measurement is made near the center of the Sq focus. In order to elucidate a mechanism to cause the electron temperature increase, the sounding rocket experiment was conducted in Uchinoura Space Center in Japan on January 16, 2007. The rocket was launched at 11:20 JST after identifying that the Sq current was approaching to the planned rocket trajectory. The rocket certainly observed the local increase of the electron temperature at the altitude of 97-101 kin. We present a preliminary analysis of the data such as the electron temperature, density, and its perturbation obtained during this campaign.
  • 今村剛, 中村正人, 上野宗孝, 佐藤毅彦, 渡部重人, 田口真, 高橋幸弘, 鈴木睦, 岩上直幹, 石井信明, 阿部琢美, 山崎敦, 福原哲哉, 上水一典, 坂野井健, 山田学, 橋本成司
    宇宙科学技術連合講演会講演集(CD-ROM) 2007年
  • 高橋幸弘, 坂野井健, 上野宗孝, 笠羽康正, 吉田和哉, 田口真, 山崎敦, 岩上直幹, 今村剛, 鈴木睦, 阿部琢美, 寺田直樹, 寺田直樹, 土屋史紀, 堀之内武, 中島健介, 高橋幸弘, 高橋幸弘
    地球電磁気・地球惑星圏学会総会及び講演会予稿集(CD-ROM) 2007年
  • 阿部琢美, 下山学, 岡田敏美, 石坂圭吾, 遠山文雄, 高橋隆男, 田中真, 湯元清文, 公田浩子, 岩満一寛, 村上尚美, 小山孝一郎
    大気圏シンポジウム 2007年
  • 坂野井健, 高橋幸弘, 上野宗孝, 笠羽康正, 吉田和哉, 山崎敦, 今村剛, 阿部琢美, 田口真, 澤井秀次郎, 高橋幸弘
    地球電磁気・地球惑星圏学会総会及び講演会予稿集(CD-ROM) 2007年
  • 横山雄生, 山本真行, 羽生宏人, 阿部琢美, 渡部重十, 池田優二
    地球電磁気・地球惑星圏学会総会及び講演会予稿集(CD-ROM) 2007年
  • 小野高幸, 渡部重十, 山本衛, 阿部琢美, 羽生宏人, 齊藤昭則, 大塚雄一, 山本真行
    地球電磁気・地球惑星圏学会総会及び講演会予稿集(CD-ROM) 2007年
  • 栗原純一, 阿部琢美, 小山孝一郎, 岩上直幹, 野澤悟徳, 小川泰信, 藤井良一, KOSCH M, GRIFFIN E, ARULIAH A, KAURISTIE K
    大気圏シンポジウム 2006年6月
  • 栗原純一, 阿部琢美, 小山孝一郎
    スペース・プラズマ研究会 2005年8月
  • 久保田実, 川村誠治, 阿保真, 内海通弘, 小泉宜子, 阿部琢美, 小山孝一郎, 塩川和夫, 大塚雄一
    日本気象学会大会講演予稿集 2005年4月30日 日本気象学会
  • Nobuaki Ishii, Yoshifumi Inatani, Satoshi Nonaka, Takashi Nakajima, Abe Takumi, Tsuda Yuichi, Takamasa Yamagami
    European Space Agency, (Special Publication) ESA SP 2005年
    In October 2003, a new space agency, JAXA (Japan Aerospace Exploration Agency) was reorganized and started as a primary space agency to promote all space activities in Japan. The Institute of Space and Astronautical Science (ISAS) belonged to JAXA and continued to promote space science and technologies using unique scientific satellites, sounding rockets and balloons. This paper summarizes sounding rocket and ballooning activities of ISAS in the fiscal year of 2003 and 2004, associated with satellite launch programs. In this time period, three sounding rockets and nineteen balloons were launched by ISAS. One of the sounding rocket, S-310-35 was an international collaboration between Japan and Norway, which was launched from Andoya Rocket Range (ARR), Andenes, Norway, so as to study the upper atmospheric dynamics and energetics associated with the auroral energy in the polar lower thermosphere. Through the combination with the national researchers and the cooperation with international organizations, ISAS will keep its own flight opportunities and be able to obtain many new scientific findings.
  • 栗原純一, 阿部琢美, 小山孝一郎
    大気圏シンポジウム 2005年
  • 中村 正人, 今村 剛, 阿部 琢美
    宇宙科学シンポジウム 2004年1月8日 相模原 : 宇宙航空研究開発機構宇宙科学研究本部
  • 阿部 琢美, 小山 孝一郎
    日本惑星科学会秋期講演会予稿集 2001年10月6日 日本惑星科学会
    We present proposals for observing the plasma transportation and circulation processes and the dynamics of the thermal plasmas that are the important element on Venus ionosphere by instruments installed on Venus Climate Orbiter. Main purpose of the observation is to elucidate the following unresolved problems: 1) How the upper atmosphere interacts with the lower atmosphere. 2) How much the energy of the solar wind can enter to the Venus upper atmosphere. 3) How momentum and energy of particles are transported into the upper atmosphere from external regions through the coupling process. In the presentation, the observation target and strategy will be discussed in detail.
  • 市川 洋一, 阿部 琢美, 小山 孝一郎
    宇宙科学シンポジウム 2001年1月11日 相模原 : 宇宙航空研究開発機構宇宙科学研究本部
    記事種別: 会議・学会報告・シンポジウム
  • 山田学, 渡部重十, 阿部琢美, 佐川永一
    地球電磁気・地球惑星圏学会総会及び講演会予稿集(CD-ROM) 2001年
  • 渡部重十, 山田学, 奥朋之, 阿部琢美, 佐川永一
    地球電磁気・地球惑星圏学会総会及び講演会予稿集(CD-ROM) 2001年

担当経験のある科目(授業)

 1

所属学協会

 3

Works(作品等)

 2

共同研究・競争的資金等の研究課題

 15
もっとみる

● 指導学生等の数

 2
  • 年度
    2021年度(FY2021)
    修士課程学生数
    4
    受託指導学生数
    4
    技術習得生の数
    1
  • 年度
    2020年度(FY2020)
    修士課程学生数
    3
    受託指導学生数
    3
    技術習得生の数
    2

● 専任大学名

 1
  • 専任大学名
    総合研究大学院大学（SOKENDAI)

● 所属する所内委員会

 3
  • 所内委員会名
    理学委員会
  • 所内委員会名
    観測ロケット専門委員会
  • 所内委員会名
    スペースチェンバー専門委員会
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