Výsledky vyhledávání - "small scientific satellite"

Overcharge tolerance test of lithium ion battery

Publikováno v: 第27回宇宙エネルギーシンポジウム平成19年度 = The Twenty-seventh Space Energy Symposium. :31-35

This study shows overcharge tolerance of lithium ion battery for ground use, in order to use it for a small satellite. Kyushu university, Kyushu institute of technology and Fukuoka institute of technology are developing a polar plasma observation sat

Externí odkaz: https://explore.openaire.eu/search/publication?articleId=jairo_______::41ee178aff7d52c30b595ae0b3a91ddf
http://id.nii.ac.jp/1696/00008014/

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Observation of auroras using the Reimei satellite

Autor: Asamura, Kazushi, Sakanoi, Takeshi, Hirahara, Masafumi, Saito, Hirobumi, INDEX Team

Publikováno v: 第7回宇宙科学シンポジウム = Proceedings of the 7th Space Science Symposium. :19-22

資料番号: AA0063354001

Externí odkaz: https://explore.openaire.eu/search/publication?articleId=jairo_______::6b20a11b99393e84ccd09010a8230652
http://id.nii.ac.jp/1696/00011146/

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Present status of development and scientific investigation of TOPS, the mission for a spaceborne planetary telescope

Autor: Takahashi, Yukihiro, Sakanoi, Takeshi, Yoshida, Kazuya, Sakamoto, Yuji, Tsuchiya, Fuminori, Taguchi, Makoto, Iwagami, Naomoto, Yamazaki, Atsushi, Terada, Naoki, Horinouchi, Takeshi

Publikováno v: 第7回宇宙科学シンポジウム = Proceedings of the 7th Space Science Symposium. :950-955

資料番号: AA0063354033

Externí odkaz: https://explore.openaire.eu/search/publication?articleId=jairo_______::2dd78c1f3d12a77a2eb1953e7749446c
http://id.nii.ac.jp/1696/00011178/

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Ground Network Observations for the ERG Project

Autor: Shiokawa, Kazuo, Nishitani, Nozomu, Kikuchi, Takashi, Otsuka, Yuichi, Miyoshi, Yoshizumi, Fujii, Ryoichi, Yumoto, Kiyofumi, Kawano, Hideaki, Yoshikawa, Akimasa, Sato, Natsuo

Publikováno v: 第7回宇宙科学シンポジウム = Proceedings of the 7th Space Science Symposium. :914-917

第10回宇宙科学シンポジウム (2010年1月7日-8日. 宇宙航空研究開発機構宇宙科学研究本部)
10th Space Science Symposium (January 7-8, 2010. Institute of Space and Astronautical Science, Japan Aerospace Exploration Agen

Externí odkaz: https://explore.openaire.eu/search/publication?articleId=dedup_wf_001::a6bcd71ac443f32279978e16096ad6b3
http://id.nii.ac.jp/1696/00011175/

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Lowering the threshold of aerospace science: Satellites. Idea of a standard satellite bus

Autor: Saito, Hirobumi

Publikováno v: 第7回宇宙科学シンポジウム = Proceedings of the 7th Space Science Symposium. :238-243

Japan Aerospace Exploration Agency has a plan to develop small satellite standard bus for various scientific mission and disaster monitoring missions. The satellite bus is a class of 200-400 Kg mass with three-axis control capability of 0.02 deg accu

Externí odkaz: https://explore.openaire.eu/search/publication?articleId=jairo_______::4e8429f43a25ba2f821dbfc88145dcc0
http://id.nii.ac.jp/1696/00011148/

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Preliminary study on thermal control system of SDS-1

Autor: Okamoto, Atsushi

Publikováno v: 宇宙航空研究開発機構特別資料: 平成18年度宇宙航空研究開発機構総合技術研究本部宇宙科学研究本部研究成果報告書 = JAXA Special Publication: Report on Research Achievements for FY2006 Institute of Space and Astronautical Science, Institute of Aerospace Technology, Japan Aerospace Exploration Agency. :227-232

In this research and development, thermal design of TCS (thermal control system) of SDS-1 is conducted. This paper describes preliminary study on the thermal design. A thermal design policy is determined, based on environmental demands for TCS, and t

Externí odkaz: https://explore.openaire.eu/search/publication?articleId=jairo_______::da472ce79561b263194979f1dfbb414a
http://id.nii.ac.jp/1696/00006028/

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Result of Micro-LabSat & future plan of small satellite

Autor: Hashimoto, Hidekazu

The Space Technology Demonstration Research Center in JAXA has researched on the potential ability of 50-100 kg class small satellites. Micro-LabSat, the first one of the series, is a 50 kg class of spin stabilized satellite launched in December 2002

Externí odkaz: https://explore.openaire.eu/search/publication?articleId=jairo_______::52ac5279fe33e35240625bd992dae547
http://id.nii.ac.jp/1696/00005979/

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In-orbit achievement of INDEX (Reimei) and future advanced function small satellites

Autor: Saito, Hirobumi, Nakamura, Masato, Yoshihara, Keisuke, Kitade, Kenji, Yasumitsu, Ryoichiro

Japan Aerospace Exploration Agency has a plan to develop small satellite standard bus for various scientific mission and disaster monitoring missions. The satellite bus is a class of 200-400 kg mass with three-axis control capability of 0.02 deg accu

Externí odkaz: https://explore.openaire.eu/search/publication?articleId=jairo_______::ae6ff2f68e365e5f03ebe97313f276be
http://id.nii.ac.jp/1696/00005981/

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Research and development of small demonstration satellite

Autor: Nakamura, Yosuke, Hirako, Keiichi, Hashimoto, Hidekazu

The Space-technology Demonstration Research Center (SDRC) of JAXA has been studying the small satellites since 1998. The circumstances surrounding the small satellite project have changed since the launch of our first satellite, MicroLabSat, in 2002.

Externí odkaz: https://explore.openaire.eu/search/publication?articleId=jairo_______::77c982418c82d0a5fb69f96fed209437
http://id.nii.ac.jp/1696/00005982/

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