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スーパーキャパシタを蓄電源に用いた宇宙機電源システム
https://jaxa.repo.nii.ac.jp/records/8017
https://jaxa.repo.nii.ac.jp/records/8017b9083ebd-9ff6-4518-83ce-d050078ca22e
Item type | 会議発表論文 / Conference Paper(1) | |||||
---|---|---|---|---|---|---|
公開日 | 2015-03-26 | |||||
タイトル | ||||||
タイトル | スーパーキャパシタを蓄電源に用いた宇宙機電源システム | |||||
言語 | ||||||
言語 | jpn | |||||
キーワード | ||||||
主題Scheme | Other | |||||
主題 | 宇宙機給電 | |||||
キーワード | ||||||
主題Scheme | Other | |||||
主題 | 蓄電池 | |||||
キーワード | ||||||
主題Scheme | Other | |||||
主題 | 加速寿命試験 | |||||
キーワード | ||||||
主題Scheme | Other | |||||
主題 | スーパーキャパシタ | |||||
キーワード | ||||||
主題Scheme | Other | |||||
主題 | DC/DCコンバータ | |||||
キーワード | ||||||
主題Scheme | Other | |||||
主題 | 太陽電池 | |||||
キーワード | ||||||
主題Scheme | Other | |||||
主題 | エネルギー変換効率 | |||||
キーワード | ||||||
主題Scheme | Other | |||||
主題 | 放電 | |||||
キーワード | ||||||
言語 | en | |||||
主題Scheme | Other | |||||
主題 | spacecraft power supply | |||||
キーワード | ||||||
言語 | en | |||||
主題Scheme | Other | |||||
主題 | storage battery | |||||
キーワード | ||||||
言語 | en | |||||
主題Scheme | Other | |||||
主題 | accelerated life test | |||||
キーワード | ||||||
言語 | en | |||||
主題Scheme | Other | |||||
主題 | supercapacitor | |||||
キーワード | ||||||
言語 | en | |||||
主題Scheme | Other | |||||
主題 | DC/DC converter | |||||
キーワード | ||||||
言語 | en | |||||
主題Scheme | Other | |||||
主題 | solar cell | |||||
キーワード | ||||||
言語 | en | |||||
主題Scheme | Other | |||||
主題 | energy conversion efficiency | |||||
キーワード | ||||||
言語 | en | |||||
主題Scheme | Other | |||||
主題 | electric discharge | |||||
資源タイプ | ||||||
資源タイプ識別子 | http://purl.org/coar/resource_type/c_5794 | |||||
資源タイプ | conference paper | |||||
アクセス権 | ||||||
アクセス権 | metadata only access | |||||
アクセス権URI | http://purl.org/coar/access_right/c_14cb | |||||
その他のタイトル(英) | ||||||
その他のタイトル | Supercapacitor-based spacecraft power system | |||||
著者 |
鵜野, 将年
× 鵜野, 将年× 豊田, 裕之× Uno, Masatoshi× Toyota, Hiroyuki |
|||||
著者所属 | ||||||
宇宙航空研究開発機構 宇宙科学研究本部 | ||||||
著者所属 | ||||||
宇宙航空研究開発機構 宇宙科学研究本部 | ||||||
著者所属(英) | ||||||
en | ||||||
Japan Aerospace Exploration Agency (JAXA) Institute of Space and Astronautical Science (ISAS) | ||||||
著者所属(英) | ||||||
en | ||||||
Japan Aerospace Exploration Agency (JAXA) Institute of Space and Astronautical Science (ISAS) | ||||||
出版者 | ||||||
出版者 | 宇宙航空研究開発機構宇宙科学研究本部 | |||||
出版者(英) | ||||||
出版者 | Institute of Space and Astronautical Science, Japan Aerospace Exploration Agency (JAXA/ISAS) | |||||
書誌情報 |
第27回宇宙エネルギーシンポジウム 平成19年度 en : The Twenty-seventh Space Energy Symposium p. 16-20, 発行日 2008-05 |
|||||
抄録(英) | ||||||
内容記述タイプ | Other | |||||
内容記述 | The power sources which have long life performances are strongly desired for deep space explorations, advanced missions and so forth. Spacecrafts ordinarily employ chemical batteries such as Ni-Cd, Ni-MH and Li-ion batteries as their power sources. Chemical batteries which store electricity by chemical reactions, however, have technical problems in the case of the very long term applications. SuperCapacitors (SCs) which are prosperously developed in the civilian field are the energy storage devices without chemical reactions. SCs have long life performances and high rate charge/discharge performances. In recent years, SCs have been applied for EVs (Electric Vehicles), UPSs (Uninterrupted Power Sources), assist power sources and so forth. In the space field, SCs were already applied to the exploration robot 'MINERVA' which was equipped to the interplanetary spacecraft 'Hayabusa (MUSES-C: Asteroid Sample-return Spacecraft)'. SCs received much attention to be applied to the very long term missions such as Space Solar Power Systems (SSPS). SCs are promising not only for commercial applications but also aerospace applications. Main drawback of SCs is that terminal voltages vary directly with stored energies. In order to adequately utilize stored energies of SCs, discharges should be as deep as possible. On the other hand, output voltage of series-connected SCs should be limited within particular range for instruments to perform appropriately. A proposed SC-based spacecraft power system is a combination of dc-dc converter and tap selector. In this paper, the power system which can utilize energies of SCs as much as possible with limiting output voltage variations within particular range is proposed and is experimentally verified using a simple circuit. Moreover, new method of controlling solar cell output power using the tap selector is also proposed. | |||||
資料番号 | ||||||
内容記述タイプ | Other | |||||
内容記述 | 資料番号: AA0063965004 |