| Item type |
学術雑誌論文 / Journal Article.(1) |
| 公開日 |
2021-03-09 |
| 書誌情報 |
en : TRANSACTIONS OF THE JAPAN SOCIETY FOR AERONAUTICAL AND SPACE SCIENCES
巻 12,
号 29,
発行日 2014
|
| タイトル |
|
|
タイトル |
Development of a Small-scale Supersonic Flight Experiment Vehicle as a Flying Test Bed for Future Space Transportation Research |
|
言語 |
en |
| 言語 |
|
|
言語 |
eng |
| キーワード |
|
|
言語 |
en |
|
主題Scheme |
Other |
|
主題 |
Space Transportation |
| キーワード |
|
|
言語 |
en |
|
主題Scheme |
Other |
|
主題 |
Flying Test Bed |
| キーワード |
|
|
言語 |
en |
|
主題Scheme |
Other |
|
主題 |
Flight Test |
| キーワード |
|
|
言語 |
en |
|
主題Scheme |
Other |
|
主題 |
Supersonic |
| キーワード |
|
|
言語 |
en |
|
主題Scheme |
Other |
|
主題 |
Jet Propulsion |
| 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 |
journal article |
| 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
湊, 亮二郎
樋口, 健
上羽, 正純
高木, 正平
中田, 大将
東野, 和幸
棚次, 亘弘
|
| 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 |
| 室蘭工業大学研究者データベースへのリンク |
|
|
|
湊 亮二郎（MINATO Ryojiro） |
|
|
http://rdsoran.muroran-it.ac.jp/html/100000234_ja.html |
| 室蘭工業大学研究者データベースへのリンク |
|
|
|
上羽 正純（UEBA Masazumi） |
|
|
http://rdsoran.muroran-it.ac.jp/html/100000004_ja.html |
| 室蘭工業大学研究者データベースへのリンク |
|
|
|
中田 大将（NAKATA Daisuke） |
|
|
http://rdsoran.muroran-it.ac.jp/html/100000232_ja.html |
| 抄録 |
|
|
内容記述タイプ |
Abstract |
|
内容記述 |
Innovation in technologies for high-speed atmospheric flights is essential for establishment of both supersonic/hypersonic and reusable space transportations. It is quite effective to verify such technologies through small-scale flight tests in practical high-speed environments, prior to installation to large-scale vehicles. Thus we are developing a small-scale supersonic flight experiment vehicle as a flying test bed. Several aerodynamic configurations are proposed and analyzed by wind tunnel tests. A twin-engine configuration with a cranked-arrow main wing is selected as the baseline of the first generation vehicle. Its flight capability is predicted by point mass analysis on the basis of aerodynamic characterization and propulsion performance estimation. In addition, a prototype vehicle with an almost equivalent configuration and dimension is designed and fabricated for verification of the subsonic flight characteristics of the experiment vehicle. Its first flight test is carried out and good flight capability is demonstrated. Furthermore a revised aerodynamic configuration with an air-turbo ramjet gas-generator cycle (ATR-GG) engine is being designed for the second generation design with improvement in flight capability at higher Mach numbers. Development of the engine, airframe structure, and autonomous guidance/control system is underway. This prospective flight experiment vehicle will be applied to flight verification of innovative fundamental technologies for high-speed atmospheric flights such as turbo-ramjet propulsion with endothermic or biomass fuels, MEMS and morphing techniques for aerodynamic control, aero-servo-elastic technologies, etc. |
|
言語 |
en |
| 出版者 |
|
|
出版者 |
JAPAN SOC AERONAUT SPACE SCI |
|
言語 |
en |
| 出版者版へのリンク |
|
|
|
10.2322/tastj.12.Po_3_1 |
|
|
https://doi.org/10.2322/tastj.12.Po_3_1 |
| DOI |
|
|
関連タイプ |
isIdenticalTo |
|
|
識別子タイプ |
DOI |
|
|
関連識別子 |
10.2322/tastj.12.Po_3_1 |
| 日本十進分類法 |
|
|
主題Scheme |
NDC |
|
主題 |
538 |
| ISSN |
|
|
収録物識別子タイプ |
EISSN |
|
収録物識別子 |
1884-0485 |
| 権利 |
|
|
言語 |
en |
|
権利情報 |
© 2014 JAPAN SOCIETY FOR AERONAUTICAL AND SPACE SCIENCES |
| 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 |
TASTJ_12_29_Po3_1_Po3_10 (4.1 MB)
