衛星/ロケット設計評価のための振動解析手法と実験的手法に関する調査・研究

Material type: 文書・図像類

Author: 下田, 孝幸ほか

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)：: This paper describes the results of an investigation into the current status of a satellite-rocket coupled load analysis technique and a vibration tes...

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Material Type: 文書・図像類
Title: 衛星/ロケット設計評価のための振動解析手法と実験的手法に関する調査・研究
Author/Editor: 下田, 孝幸
内田, 英樹
幸節, 雄二
Shimoda, Takayuki
Uchida, Hideki
Kosetsu, Yuji
Author Heading: 下田, 孝幸
内田, 英樹
幸節, 雄二
Shimoda, Takayuki
Uchida, Hideki
Kosetsu, Yuji
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: Coupled load analysis and testing method for evaluating design of satellite/rocket
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:人工衛星系基盤技術 = 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 Satellite Systems
No. or year of volume/issue: JAXA-SP-05-008
Volume: JAXA-SP-05-008
Pages: 31-36
ISSN (Periodical Title): ISSN : 1349-113X
Text Language Code: jpn
Subject Heading: 衛星設計
ロケットエンジン設計
振動荷重
結合振動荷重解析
数学モデル
計算機プログラム
構造設計
振動試験
satellite design
rocket engine design
vibratory load
coupled load analysis
mathematical model
computer program
structural design
vibration test
Target Audience: 一般
Note (General): This paper describes the results of an investigation into the current status of a satellite-rocket coupled load analysis technique and a vibration test technique used to validate analytical results in Europe and the USA. Their analytical techniques are at the same level as in Japan. They consider vibration testing to be important for validating analysis results but believe that it is difficult to validate results by testing with a three-axis, six-DOF test machine. A Japanese manufacturer has a good technology for performing such tests. We concluded that Japan has the potential to lead other countries in this technical area by realizing a three-axis, six-DOF test machine for analyzing and improving coupled load methods.
資料番号: AA0049054007
レポート番号: JAXA-SP-05-008
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