マイクロラブサットシリーズの成果と展望:1号機の成果と2号機設計状況

Material type: 文書・図像類

Author: 立原, 裕司ほか

Publisher: 宇宙航空研究開発機構

Publication date: 2004-10-29

Material Format: Digital

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Note (General)：: The Space Technology Demonstration Research Center in JAXA has researched on the development of 50 to 100 kg class small satellites which is used to c...

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Material Type: 文書・図像類
Title: マイクロラブサットシリーズの成果と展望:1号機の成果と2号機設計状況
Author/Editor: 立原, 裕司
高橋, 伸宏
吉原, 圭介
橋本, 英一
Tachihara, Hiroshi
Takahashi, Nobuhiro
Yoshihara, Keisuke
Hashimoto, Hidekazu
Author Heading: 立原, 裕司
高橋, 伸宏
吉原, 圭介
橋本, 英一
Tachihara, Hiroshi
Takahashi, Nobuhiro
Yoshihara, Keisuke
Hashimoto, Hidekazu
Publication, Distribution, etc.: 宇宙航空研究開発機構
Publication Date: 2004-10-29
Publication Date (W3CDTF): 2004-10-29
Alternative Title: Fruitful results of MicroLabSat and ambitious development of MicroLabSat 2
Periodical title: 宇宙航空研究開発機構研究開発資料: 平成15年度総合技術研究本部宇宙領域研究成果報告書:衛星系 = JAXA Research and Development Memorandum: FY15 Annual Report of Research & Development on Space Technology in the Institute of Space Technology and Aeronautics: Satellite System
No. or year of volume/issue: JAXA-RM-04-010
Volume: JAXA-RM-04-010
Pages: 109-114
ISSN (Periodical Title): ISSN : 1349-1121
Text Language Code: jpn
Subject Heading: MicroLabSat-2
H-2Aロケット
姿勢制御
マイクロ衛星
ピギーバックシステム
Ni-MH電池
磁気嵐
衛星通信
H-2A rocket
attitude control
microsatellite
piggyback system
Ni-MH battery
magnetic storm
satellite communication
Target Audience: 一般
Note (General): The Space Technology Demonstration Research Center in JAXA has researched on the development of 50 to 100 kg class small satellites which is used to carry newly-developed components and devices into space and to check their normal work. There is a plan to develop several types of such small 'space demonstration satellites' as a series. MicroLabSat, the first one of the series, is a 50 kg class of spin stabilized satellite launched in December 2002 as a piggy back satellite on H-2A rocket. It has successfully completed all the planned experiments and continues healthy operation. Following MicroLabSat, MicroLabSat 2 is being developed with the three axis stabilized attitude control system. The results of two satellites will be brought into the following space demonstration satellites of the series. The fruitful results of MicroLabSat and the recent status of developing MicroLabSat 2 will be expressed in this paper.
資料番号: AA0048057023
レポート番号: JAXA-RM-04-010
Source: https://jaxa.repo.nii.ac.jp/?action=repository_action_common_download&item_id=2714&item_no=1&attribute_id=31&file_no=1
https://jaxa.repo.nii.ac.jp/?action=repository_action_common_download&item_id=2714&item_no=1&attribute_id=31&file_no=1
Access Restrictions: 限定公開
Data Provider (Database): 国立情報学研究所 : 学術機関リポジトリデータベース（IRDB）（機関リポジトリ）
https://irdb.nii.ac.jp
Original Data Provider (Database): 宇宙航空研究開発機構 : 宇宙航空研究開発機構リポジトリ