並列タイトル等Evaluation of New Type Stress Sensor Capable of Measuring Radial Bond Stresses Between Solid Propellant and Rocket Motor Case
タイトル(掲載誌)航空宇宙技術研究所資料 = Technical Memorandum of National Aerospace Laboratory
一般注記For the purpose of measuring the radial bond stresses between the solid propellant and the rocket motor case, a new type of stress measuring sensor was made and tested. The sensor is an application of a diaphragm type small size pressure transducer using electric foil strain gages. The input-output relations of the sensor, including its tem- perature characteristics, were examined. Numerical solutions were also obtained by the finite element method. It was found that there was a satisfactory argreement of the bond stresses between the test results and the numerical solution.
資料番号: NALTM0209000
レポート番号: NAL TM-209
一次資料へのリンクURLhttps://jaxa.repo.nii.ac.jp/?action=repository_action_common_download&item_id=43793&item_no=1&attribute_id=31&file_no=1
連携機関・データベース国立情報学研究所 : 学術機関リポジトリデータベース(IRDB)(機関リポジトリ)
提供元機関・データベース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