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  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)

衛星用再突入時溶融促進型推進薬タンクの試作#1開発状況

https://jaxa.repo.nii.ac.jp/records/38653
https://jaxa.repo.nii.ac.jp/records/38653
ad59996c-de1e-4161-b91d-98f393e3131f
Item type 会議発表論文 / Conference Paper(1)
公開日 2015-04-22
タイトル
タイトル 衛星用再突入時溶融促進型推進薬タンクの試作#1開発状況
言語
言語 jpn
キーワード
言語 en
主題Scheme Other
主題 Tank
キーワード
言語 en
主題Scheme Other
主題 Propellant
キーワード
言語 en
主題Scheme Other
主題 Re-entry
キーワード
言語 en
主題Scheme Other
主題 Propulsion system
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 The development of Trial #1 Reentry Melting Promotion Propellant tank.
著者 山田, 啓介

× 山田, 啓介

WEKO 435354

山田, 啓介

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石田, 大二郎

× 石田, 大二郎

WEKO 435355

石田, 大二郎

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升岡, 正

× 升岡, 正

WEKO 435356

升岡, 正

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増田, 井出夫

× 増田, 井出夫

WEKO 435357

増田, 井出夫

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池田, 博英

× 池田, 博英

WEKO 435358

池田, 博英

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Yamada, Keisuke

× Yamada, Keisuke

WEKO 435359

en Yamada, Keisuke

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Ishida, Daijirou

× Ishida, Daijirou

WEKO 435360

en Ishida, Daijirou

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Masuoka, Tadashi

× Masuoka, Tadashi

WEKO 435361

en Masuoka, Tadashi

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Masuda, Ideo

× Masuda, Ideo

WEKO 435362

en Masuda, Ideo

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Ikeda, Hirohide

× Ikeda, Hirohide

WEKO 435363

en Ikeda, Hirohide

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著者所属
IHIエアロスペース
著者所属
IHIエアロスペース
著者所属
宇宙航空研究開発機構(JAXA)
著者所属
宇宙航空研究開発機構(JAXA)
著者所属
宇宙航空研究開発機構(JAXA)
著者所属(英)
en
IHI AEROSPACE
著者所属(英)
en
IHI AEROSPACE
著者所属(英)
en
Japan Aerospace Exploration Agency(JAXA)
著者所属(英)
en
Japan Aerospace Exploration Agency(JAXA)
著者所属(英)
en
Japan Aerospace Exploration Agency(JAXA)
出版者
出版者 日本航空宇宙学会(JSASS)
出版者(英)
出版者 The Japan Society for Aeronautical and Space Sciences (JSASS)
書誌情報 第58回宇宙科学技術連合講演会講演集
en : Proceedings of 58th Space Sciences and Technology Conference

発行日 2014-11
会議概要(会議名, 開催地, 会期, 主催者等)
内容記述タイプ Other
内容記述 第58回宇宙科学技術連合講演会(2014年11月12日-14日. 長崎ブリックホール), 長崎市, 長崎県
抄録(英)
内容記述タイプ Other
内容記述 The component of a satellite falling to the ground is a crucial problem, since titanium tanks are one of the components causing most damage to the ground in satellites. To replace titanium tanks, JAXA has researched a Melting Promotion Type Tank which can reduce residual debris during the re-entry phase. The tank structure features an aluminum liner overwrapped with carbon composite (filament winding). This paper summarizes the trial #1 tank & PMD (Propellant Management Device) manufacture and tests.
資料番号
内容記述タイプ Other
内容記述 資料番号: AC1500012000
レポート番号
内容記述タイプ Other
内容記述 レポート番号: JSASS-2014-4201
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