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規格・テクニカルリポート類

極超音速実験機(HYFLEX)設計結果

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極超音速実験機(HYFLEX)設計結果

Material type
規格・テクニカルリポート類
Author
白水, 正男ほか
Publisher
航空宇宙技術研究所
Publication date
2003-08
Material Format
Digital
Capacity, size, etc.
-
NDC
-
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Notes on use

Note (General):

The Hypersonic Flight Experiment (HYFLEX) was conducted in February 1996 as Japan's first hypersonic flight of a lifting vehicle with the basic charac...

Detailed bibliographic record

Summary, etc.:

1996年に飛行実験を行った極超音速飛行実験(HYFLEX)の最終的な設計結果について、全体像をまとめた。この飛行実験は日本初の極超音速揚力飛行であり、機体や飛行計画は宇宙往還機の基本的な特徴を有する。記述は機体の設計を中心とし、サブシステム毎に設計結果やその考え方などを詳述し、飛行計画やデータ解析...

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Bibliographic Record

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Digital

Material Type
規格・テクニカルリポート類
Author/Editor
白水, 正男
渡辺, 重哉
滝沢, 実
甲斐, 高志
高木, 亮治
鈴木, 広一
伊藤, 健
寺岡, 謙
NAL/NASDA HOPE研究共同チーム
Shirouzu, Masao
Watanabe, Shigeya
Takizawa, Minoru
Kai, Takashi
Takaki, Ryoji
Suzuki, Hirokazu
Ito, Takeshi
Teraoka, Ken
NAL/NASDA HOPE Team
Publication, Distribution, etc.
Publication Date
2003-08
Publication Date (W3CDTF)
2003-08
Alternative Title
Design and development of the Hypersonic Flight Experiment (HYFLEX) vehicle
Periodical title
航空宇宙技術研究所報告
No. or year of volume/issue
1466
Volume
1466
ISSN (Periodical Title)
ISSN : 1347-4588
Text Language Code
jpn
Target Audience
一般
Note (General)
The Hypersonic Flight Experiment (HYFLEX) was conducted in February 1996 as Japan's first hypersonic flight of a lifting vehicle with the basic characteristics of a reentry vehicle. This paper describes details of the final design of the vehicle sub-systems, and in brief its flight plan and an analysis of the flight data.
資料番号: AA0047386000
レポート番号: NAL TR-1466
Access Restrictions
インターネット公開
Data Provider (Database)
国立情報学研究所 : 学術機関リポジトリデータベース(IRDB)(機関リポジトリ)
Original Data Provider (Database)
宇宙航空研究開発機構 : 宇宙航空研究開発機構リポジトリ