再突入カプセルの高エンタルピ空力加熱試験

Material type: 文書・図像類

Author: 橋本, 時忠ほか

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)：: In recent years, development of re-usable space transportation system is promoted. However, in order to realize it, development of the base technology...

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Material Type: 文書・図像類
Title: 再突入カプセルの高エンタルピ空力加熱試験
Author/Editor: 橋本, 時忠
小室, 智幸
高橋, 政浩
佐藤, 和雄
伊藤, 勝宏
Hashimoto, Tokitada
Komuro, Tomoyuki
Takahashi, Masahiro
Sato, Kazuo
Ito, Katsuhiro
Author Heading: 橋本, 時忠
小室, 智幸
高橋, 政浩
佐藤, 和雄
伊藤, 勝宏
Hashimoto, Tokitada
Komuro, Tomoyuki
Takahashi, Masahiro
Sato, Kazuo
Ito, Katsuhiro
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: High enthalpy aerodynamic heating experiments over a reentry capsule
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: 89-92
ISSN (Periodical Title): ISSN : 1349-113X
Text Language Code: jpn
Subject Heading: 高エンタルピ衝撃風洞
空力加熱
再使用型打上げ機
大気圏再突入
再突入機
熱伝達
宇宙カプセル
鈍頭体
圧力分布
流れの分布
計算機シミュレーション
high enthalpy shock tunnel
aerodynamic heating
reusable launch vehicle
atmospheric reentry
reentry vehicle
heat transfer
space capsule
blunt body
pressure distribution
flow distribution
computerized simulation
Target Audience: 一般
Note (General): In recent years, development of re-usable space transportation system is promoted. However, in order to realize it, development of the base technology is indispensable, particularly, aerodynamic heating and characteristics with strong real gas phenomena should be comprehended more precisely. Under such circumstances, acquisition of detailed experimental data like drag and heat transfer over hypersonic bodies is indispensable for the development of reliable space vehicles and thermal protection system (TPS), and also for the validation and progress of numerical estimation. In the present study, based on the numerical results a blunted double cone model (heat model) was designed and manufactured as the aerodynamic configuration design of re-entry capsules. The aim of this experiment is to obtain detailed data of heat flux and pressure distribution as well as the flow structures over the heat model. Coaxial thermocouples and pressure sensors are mounted at the frontal and base region thoroughly, and surface temperature and wall pressure are measured.
資料番号: AA0049500019
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