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  1. シンポジウム・研究会
  2. 宇宙エネルギーシンポジウム
  3. 第27回
  1. コンテンツタイプ
  2. 会議発表論文/会議発表用資料 (Conference Paper/Presentation)

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/8017
b9083ebd-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

WEKO 43872

鵜野, 将年

Search repository
豊田, 裕之

× 豊田, 裕之

WEKO 43873

豊田, 裕之

Search repository
Uno, Masatoshi

× Uno, Masatoshi

WEKO 43874

en Uno, Masatoshi

Search repository
Toyota, Hiroyuki

× Toyota, Hiroyuki

WEKO 43875

en Toyota, Hiroyuki

Search repository
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
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