システム解析の研究:コンセプトスタディプログラムの開発および空力技術に関する研究

Material type: 文書・図像類

Author: 鈴木, 広一ほか

Publisher: 宇宙航空研究開発機構

Publication date: 2006-01-20

Material Format: Digital

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Note (General)：: In this research, optimal design, evaluation, and aerodynamic problems for future space transportation systems are conducted. A conceptual design tool...

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Material Type: 文書・図像類
Title: システム解析の研究:コンセプトスタディプログラムの開発および空力技術に関する研究
Author/Editor: 鈴木, 広一
高嵜, 浩一
岩田, 創
苅田, 丈士
甲斐, 高志
南, 吉紀
小林, 弘明
黒滝, 卓司
Suzuki, Hirokazu
Takasaki, Koichi
Iwata, Takumi
Kanda, Takeshi
Kai, Takashi
Minami, Yoshinori
Kobayashi, Hiroaki
Kurotaki, Takuji
Author Heading: 鈴木, 広一
高嵜, 浩一
岩田, 創
苅田, 丈士
甲斐, 高志
南, 吉紀
小林, 弘明
黒滝, 卓司
Suzuki, Hirokazu
Takasaki, Koichi
Iwata, Takumi
Kanda, Takeshi
Kai, Takashi
Minami, Yoshinori
Kobayashi, Hiroaki
Kurotaki, Takuji
Publication, Distribution, etc.: 宇宙航空研究開発機構
Publication Date: 2006-01-20
Publication Date (W3CDTF): 2006-01-20
Alternative Title: Research on system analysis: Development of concept study program and research on aerodynamic technologies
Periodical title: 宇宙航空研究開発機構特別資料: 平成16年度総合技術研究本部宇宙領域宇宙科学研究本部合同研究成果報告書:宇宙輸送系基盤技術 = JAXA Special Publication: FY2004 Report of Joint Research Achievements of the Space Division of Institute of Aerospace Technology and Institute of Space and Astronautical Science: Basic Technologies of Space Transportation Systems
No. or year of volume/issue: JAXA-SP-05-010
Volume: JAXA-SP-05-010
Pages: 31-34
ISSN (Periodical Title): ISSN : 1349-113X
Text Language Code: jpn
Subject Heading: 宇宙輸送システム
概念設計
設計最適化
システム解析
触媒
空力加熱
風洞試験
CFD
space transportation system
concept design
design optimization
systems analysis
catalyst
aerodynamic heating
wind tunnel test
Target Audience: 一般
Note (General): In this research, optimal design, evaluation, and aerodynamic problems for future space transportation systems are conducted. A conceptual design tool for space transportation systems called SEAT (Systems Evaluation and Analysis Tool) is under developing. The design criteria are also investigated and several types of the concept for the future space transportation systems are designed optimally and are evaluated. In the last fiscal year, a prototype of the SEAT was developed. The catalysis is dealt as aerodynamic problems for the future space transportation systems. In the last fiscal year, experimental data of various flow conditions were obtained in new ICP-heated wind tunnel.
資料番号: AA0049056006
レポート番号: JAXA-SP-05-010
Source: https://jaxa.repo.nii.ac.jp/?action=repository_action_common_download&item_id=6237&item_no=1&attribute_id=31&file_no=1
https://jaxa.repo.nii.ac.jp/?action=repository_action_common_download&item_id=6237&item_no=1&attribute_id=31&file_no=1
Access Restrictions: 限定公開
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）
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