| タイトル | ATI SAA Annex 3 Button Tensile Test Report I |
| 本文（外部サイト） | http://hdl.handle.net/2060/20140011734 |
| 著者（英） | Tang, Henry H. |
| 発行日 | 2013-11-30 |
| 言語 | eng |
| 内容記述 | This report documents the results of a study carried out under Splace Act Agreement SAA-EA-10-004 between the National Aeronautics and Space Administration (NASA) and Astro Technology Incorpporated (ATI). NASA and ATI have entered into this agreement to collaborate on the development of technologies that can benefit both the US government space programs and the oil and gas industry. The report documents the results of a test done on an adnesive system for attaching new monitoring sensor devices to pipelines under Annex III of SAA-EA-10-004: "Proof-of-Concept Design and Testing of a Post Installed Sensing Device on Subsea Risers and Pipelines". The tasks of Annex III are to design and test a proof-of-concept sensing device for in-situ installation on pipelines, risers, or other structures deployed in deep water. The function of the sensor device is to measure various signals such as strain, stress and temperature. This study complements the work done, in Annex I of the SAA, on attaching a fiber optic sensing device to pipe via adhesive bonding. Both Annex I and Annex III studies were conducted in the Crew and Thermal System Division (CTSD) at the Johnson Space Center (JSC) in collaboration with ATI. |
| NASA分類 | Mechanical Engineering |
| レポートNO | JSC-CN-30335
CTSD-ADV-1102 |
| 権利 | Copyright, Distribution under U.S. Government purpose rights |
|
