リフティングボディ飛行実験計画について:小型制御研究機の研究

Material type: 文書・図像類

Author: 塚本, 太郎ほか

Publisher: 宇宙航空研究開発機構

Publication date: 2006-11-01

Material Format: Digital

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Note (General)：: The Institute of Space Technology and Aeronautics has investigated various concepts of next generation reusable space transportation systems. Lifting-...

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Material Type: 文書・図像類
Title: リフティングボディ飛行実験計画について:小型制御研究機の研究
Author/Editor: 塚本, 太郎
南, 吉紀
山本, 行光
栗田, 充
青木, 良尚
石川, 和敏
冨田, 博史
元田, 敏和
Tsukamoto, Taro
Minami, Yoshinori
Yamamoto, Yukimitsu
Kurita, Mitsuru
Aoki, Yoshihisa
Ishikawa, Kazutoshi
Tomita, Hiroshi
Motoda, Toshikazu
Author Heading: 塚本, 太郎
南, 吉紀
山本, 行光
栗田, 充
青木, 良尚
石川, 和敏
冨田, 博史
元田, 敏和
Tsukamoto, Taro
Minami, Yoshinori
Yamamoto, Yukimitsu
Kurita, Mitsuru
Aoki, Yoshihisa
Ishikawa, Kazutoshi
Tomita, Hiroshi
Motoda, Toshikazu
Publication, Distribution, etc.: 宇宙航空研究開発機構
Publication Date: 2006-11-01
Publication Date (W3CDTF): 2006-11-01
Alternative Title: Lifting-body flight experiment project: Study of small control research vehicle
Periodical title: 宇宙航空研究開発機構特別資料: 平成18年度　宇宙航空研究開発機構　総合技術研究本部　宇宙科学研究本部　研究成果報告書 = JAXA Special Publication: Report on Research Achievements for FY2006 Institute of Space and Astronautical Science, Institute of Aerospace Technology, Japan Aerospace Exploration Agency
No. or year of volume/issue: JAXA-SP-06-006
Volume: JAXA-SP-06-006
Pages: 117-118
ISSN (Periodical Title): ISSN : 1349-113X
Text Language Code: jpn
Subject Heading: 研究機
リフティングボディ
飛行実験
空力加熱
空力特性
飛行制御
自動着陸
極超音速飛行
ヘリコプタ
research vehicle
lifting body
flight experiment
aerodynamic heating
aerodynamic characteristic
flight control
automatic landing
hypersonic flight
helicopter
Target Audience: 一般
Note (General): The Institute of Space Technology and Aeronautics has investigated various concepts of next generation reusable space transportation systems. Lifting-body re-entry vehicle is one of the most promising concepts among them. This type of vehicle has no wings and derives its lift solely from the shape of its body, and has the advantages of reduced structural weight, superior volumetric efficiency, and better characteristics against aerodynamic heating at hypersonic speed. On the other hand, the disadvantages of its low lift-drag ratio, poor stability and controllability at low speed makes it more difficult to land on a conventional runway than in the case of a winged vehicle like in the Automatic Landing Flight Experiment (ALFLEX), which conducted in 1996. In this report, we introduce the outline of the intended Lifting-body Flight Experiment (LIFLEX), which aims to gain the automatic landing technology using a small, low-cost system.
資料番号: AA0049500025
レポート番号: JAXA-SP-06-006
Access Restrictions: 限定公開
Periodical Title (NCID): AA11984031
https://ci.nii.ac.jp/ncid/AA11984031
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）
https://irdb.nii.ac.jp
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