Fruitful results of MicroLabSat and ambitious development of MicroLabSat 2
| Autor: | Tachihara, Hiroshi, Takahashi, Nobuhiro, Yoshihara, Keisuke, Hashimoto, Hidekazu |
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| Jazyk: | japonština |
| Rok vydání: | 2004 |
| Předmět: | |
| Zdroj: | 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. :109-114 |
| ISSN: | 1349-1121 |
| Popis: | 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 |
| Databáze: | OpenAIRE |
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