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再使用型有翼ハイブリットロケットシステムの基本設計と飛行性能予測
http://hdl.handle.net/10258/118
http://hdl.handle.net/10258/11840144a29-516c-4087-b7d1-7b3412e39137
名前 / ファイル | ライセンス | アクション |
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51-91.pdf (4.5 MB)
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Item type | 紀要論文 / Departmental Bulletin Paper(1) | |||||||||||||||||
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公開日 | 2007-06-06 | |||||||||||||||||
タイトル | ||||||||||||||||||
言語 | ja | |||||||||||||||||
タイトル | 再使用型有翼ハイブリットロケットシステムの基本設計と飛行性能予測 | |||||||||||||||||
タイトル | ||||||||||||||||||
言語 | en | |||||||||||||||||
タイトル | Baseline Design and Flight Capability Predictions for a Reusable Winged Hybrid Rocket System | |||||||||||||||||
言語 | ||||||||||||||||||
言語 | jpn | |||||||||||||||||
キーワード | ||||||||||||||||||
言語 | en | |||||||||||||||||
主題Scheme | Other | |||||||||||||||||
主題 | hybrid rockets | |||||||||||||||||
キーワード | ||||||||||||||||||
言語 | en | |||||||||||||||||
主題Scheme | Other | |||||||||||||||||
主題 | reusable launch system | |||||||||||||||||
キーワード | ||||||||||||||||||
言語 | en | |||||||||||||||||
主題Scheme | Other | |||||||||||||||||
主題 | flight trajectory analysis | |||||||||||||||||
資源タイプ | ||||||||||||||||||
資源タイプ識別子 | http://purl.org/coar/resource_type/c_6501 | |||||||||||||||||
資源タイプ | departmental bulletin paper | |||||||||||||||||
アクセス権 | ||||||||||||||||||
アクセス権 | open access | |||||||||||||||||
アクセス権URI | http://purl.org/coar/access_right/c_abf2 | |||||||||||||||||
著者 |
溝端, 一秀
× 溝端, 一秀
WEKO
801
× 中谷, 淳× 成田, 志門× 吉田, 拓史× 杉山, 弘
WEKO
489
× 永田, 晴紀× 伊藤, 献一× 秋葉, 鐐二郎× 大和田, 陽一 |
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室蘭工業大学研究者データベースへのリンク | ||||||||||||||||||
溝端 一秀(MIZOBATA Kazuhide) | ||||||||||||||||||
http://rdsoran.muroran-it.ac.jp/html/100000207_ja.html | ||||||||||||||||||
抄録 | ||||||||||||||||||
内容記述タイプ | Abstract | |||||||||||||||||
内容記述 | Hybrid rocket motors, propelled by a combination of a solid fuel and a liquid oxidizer, are best suited to development of small launch systems in university laboratories, becauee af their advantageous characteristics such as Bafety, easy handling. and law costs. The performance of hybrid rocket motors of three classes of thrust - 10tonf, 1tonf, and 200kgf - is estimated. The feasibility of reusable winged launch systems based on the three motors is prelirninarily analyzed for suborbital micro-gravity experiments. The results tell that a sysbem with a 10tonf-class motor by a coolant bleed cycle with polystyrene and LOx fed by an LE-5B turbopump will be capabre of exposing a payload of 360kg to a micro-gravity environment for three minutes. It is also predictied that a system with a 1tonf-class motor will be moderately capable and that with a 200kgf-class motor will not be feasible for micro gravity missions mainly because the weight of its helium pressurization system for feeding LOx will reduce the mass fraction. | |||||||||||||||||
言語 | en | |||||||||||||||||
書誌情報 |
ja : 室蘭工業大学紀要 en : Memoirs of the Muroran Institute of Technology 巻 51, p. 91-97, 発行日 2001-11-30 |
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注記 | ||||||||||||||||||
内容記述タイプ | Other | |||||||||||||||||
内容記述 | 小特集 : 「室蘭工大における航空宇宙工学研究の新展開」 | |||||||||||||||||
言語 | ja | |||||||||||||||||
出版者 | ||||||||||||||||||
言語 | ja | |||||||||||||||||
出版者 | 室蘭工業大学 | |||||||||||||||||
論文ID(NAID) | ||||||||||||||||||
関連タイプ | isIdenticalTo | |||||||||||||||||
識別子タイプ | NAID | |||||||||||||||||
関連識別子 | 110000076575 | |||||||||||||||||
日本十進分類法 | ||||||||||||||||||
主題Scheme | NDC | |||||||||||||||||
主題 | 538 | |||||||||||||||||
ISSN | ||||||||||||||||||
収録物識別子タイプ | PISSN | |||||||||||||||||
収録物識別子 | 13442708 | |||||||||||||||||
書誌レコードID | ||||||||||||||||||
収録物識別子タイプ | NCID | |||||||||||||||||
収録物識別子 | AA11175464 | |||||||||||||||||
権利 | ||||||||||||||||||
言語 | ja | |||||||||||||||||
権利情報 | © 2001 室蘭工業大学 | |||||||||||||||||
著者版フラグ | ||||||||||||||||||
出版タイプ | VoR | |||||||||||||||||
出版タイプResource | http://purl.org/coar/version/c_970fb48d4fbd8a85 | |||||||||||||||||
フォーマット | ||||||||||||||||||
内容記述タイプ | Other | |||||||||||||||||
内容記述 | application/pdf |