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宇宙往還機開発計画の概要
https://jaxa.repo.nii.ac.jp/records/36840
https://jaxa.repo.nii.ac.jp/records/36840dfde9231-9eb9-4ff4-ac48-11b50135d7d7
名前 / ファイル | ライセンス | アクション |
---|---|---|
nalsp0032001.pdf (1.6 MB)
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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 | 宇宙往還機開発計画の概要 | |||||
言語 | ||||||
言語 | jpn | |||||
キーワード | ||||||
主題Scheme | Other | |||||
主題 | 宇宙往還技術試験機 | |||||
キーワード | ||||||
主題Scheme | Other | |||||
主題 | HOPE-X | |||||
キーワード | ||||||
主題Scheme | Other | |||||
主題 | 軌道再突入実験 | |||||
キーワード | ||||||
主題Scheme | Other | |||||
主題 | OREX | |||||
キーワード | ||||||
主題Scheme | Other | |||||
主題 | 極超音速飛行実験 | |||||
キーワード | ||||||
主題Scheme | Other | |||||
主題 | HYFLEX | |||||
キーワード | ||||||
主題Scheme | Other | |||||
主題 | 小型自動着陸実験 | |||||
キーワード | ||||||
主題Scheme | Other | |||||
主題 | ALFLEX | |||||
キーワード | ||||||
主題Scheme | Other | |||||
主題 | 誘導制御 | |||||
キーワード | ||||||
主題Scheme | Other | |||||
主題 | 耐熱構造 | |||||
キーワード | ||||||
主題Scheme | Other | |||||
主題 | 再使用機 | |||||
キーワード | ||||||
主題Scheme | Other | |||||
主題 | J-1ロケット | |||||
キーワード | ||||||
主題Scheme | Other | |||||
主題 | H-2Aロケット | |||||
キーワード | ||||||
主題Scheme | Other | |||||
主題 | H-2ロケット打上げ型有翼宇宙往還機 | |||||
キーワード | ||||||
主題Scheme | Other | |||||
主題 | HOPE | |||||
キーワード | ||||||
言語 | en | |||||
主題Scheme | Other | |||||
主題 | H 2 orbiting plane experimental program | |||||
キーワード | ||||||
言語 | en | |||||
主題Scheme | Other | |||||
主題 | HOPE X | |||||
キーワード | ||||||
言語 | en | |||||
主題Scheme | Other | |||||
主題 | orbit reentry experiment | |||||
キーワード | ||||||
言語 | en | |||||
主題Scheme | Other | |||||
主題 | OREX | |||||
キーワード | ||||||
言語 | en | |||||
主題Scheme | Other | |||||
主題 | hypersonic flight experimental | |||||
キーワード | ||||||
言語 | en | |||||
主題Scheme | Other | |||||
主題 | HYFLEX | |||||
キーワード | ||||||
言語 | en | |||||
主題Scheme | Other | |||||
主題 | automatic landing flight experiment | |||||
キーワード | ||||||
言語 | en | |||||
主題Scheme | Other | |||||
主題 | ALFLEX | |||||
キーワード | ||||||
言語 | en | |||||
主題Scheme | Other | |||||
主題 | navigation control | |||||
キーワード | ||||||
言語 | en | |||||
主題Scheme | Other | |||||
主題 | heat resistant structure | |||||
キーワード | ||||||
言語 | en | |||||
主題Scheme | Other | |||||
主題 | reusable vehicle | |||||
キーワード | ||||||
言語 | en | |||||
主題Scheme | Other | |||||
主題 | J 1 rocket | |||||
キーワード | ||||||
言語 | en | |||||
主題Scheme | Other | |||||
主題 | H 2A rocket | |||||
キーワード | ||||||
言語 | en | |||||
主題Scheme | Other | |||||
主題 | H 2 orbiting plane | |||||
キーワード | ||||||
言語 | en | |||||
主題Scheme | Other | |||||
主題 | HOPE | |||||
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 | |||||
その他のタイトル(英) | ||||||
その他のタイトル | Overview of spaceplane development plan at NAL/NASDA | |||||
著者 |
山本, 昌孝
× 山本, 昌孝× Yamamoto, Masataka |
|||||
著者所属 | ||||||
宇宙開発事業団 | ||||||
著者所属(英) | ||||||
en | ||||||
National Space Development Agency of Japan | ||||||
出版者 | ||||||
出版者 | 航空宇宙技術研究所 | |||||
出版者(英) | ||||||
出版者 | National Aerospace Laboratory (NAL) | |||||
書誌情報 |
航空宇宙技術研究所特別資料 en : Special Publication of National Aerospace Laboratory 巻 32, p. 1-4, 発行日 1996-09 |
|||||
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 | 24-25 Jul. 1996 | |||||
会議概要(会議名, 開催地, 会期, 主催者等)(英) | ||||||
内容記述タイプ | Other | |||||
内容記述 | 24-25 Jul. 1996 | |||||
抄録 | ||||||
内容記述タイプ | Abstract | |||||
内容記述 | 宇宙技術研究所(NAL)と宇宙開発事業団(NASDA)は協力して、宇宙往還技術試験機(HOPE-X)の開発を進めている。開発は次項の経緯で進められた。(1)1980年代前半から空力、誘導制御、耐熱構造に関する研究、要素の試作試験を開始、(2)1980年後半から10トン級HOPE(H-2ロケット打上げ型有翼宇宙往還機)の概念設計を開始、(3)1994年2月に最初の実験機として軌道再突入実験機(OREX)をH-2ロケットによって打上げた、(4)1996年2月に極超音速飛行実験機(HYFLEX)をJ-1ロケットによって打上げた、(5)1996年より小型自動着陸(ALFLEX)はオーストラリアで飛行試験を続行中、(6)並行して打上げロケットの開発を進め、H-2Aロケットにまで高度化が進展している。HOPE-Xは、2000年度に実験を行うこととして開発を進め、近い将来に、完全再使用型宇宙往還機「HOPE」を目指す。 | |||||
抄録(英) | ||||||
内容記述タイプ | Other | |||||
内容記述 | H-2 Orbiting Plane-experimental (HOPE-X) program has been developing as a joint collaboration between National Aerospace Laboratory (NAL) and National Space Development Agency of Japan (NASDA). The following development histories of HOPE (H-2 Orbiting Plane) are described: (1) in the first half of 1980, research and development of aerodynamics, guidance/control, heat resistant structure, and components test were begun; (2) in the latter half of 1980, conceptual design of ten tons class HOPE were begun; (3) in Feb. 1994, Orbit Reentry-Experimental (OREX) vehicle were launched by H-2 rocket; (4) in Feb. 1996, Hypersonic Flight-Experimental (HYFLEX) vehicle was launched by J-1 rocket; (5) since 1996, flight test of Automatic Landing Flight-Experimental (ALFLEX) vehicle has been going on in Australia; and (6) simultaneously, development of launching rockets has been in progress to realize H-2A rocket with high performance. The HOPE-X is being developed to perform a flight test in 2000. HOPE is expected to be a perfect reusable orbiting plane. | |||||
ISSN | ||||||
収録物識別子タイプ | ISSN | |||||
収録物識別子 | 0289-260X | |||||
書誌レコードID | ||||||
収録物識別子タイプ | NCID | |||||
収録物識別子 | AN10097345 | |||||
資料番号 | ||||||
内容記述タイプ | Other | |||||
内容記述 | 資料番号: AA0000584001 | |||||
レポート番号 | ||||||
内容記述タイプ | Other | |||||
内容記述 | レポート番号: NAL SP-32 |