9 November 2000 Strain and temperature monitoring in composite sandwich panels in space environment
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Proceedings Volume 4185, Fourteenth International Conference on Optical Fiber Sensors; 41851C (2000) https://doi.org/10.1117/12.2302191
Event: Fourteenth International Conference on Optical Fiber Sensors, 2000, Venice, Italy
Abstract
To develop a health monitoring system for satellite, FBG sensor was applied to a composite panel with heat-pipe. Temperature and strain in the panel were successfully measured during thermallvacuum test in a vacuum thermal chamber.
© (2000) COPYRIGHT Society of Photo-Optical Instrumentation Engineers (SPIE). Downloading of the abstract is permitted for personal use only.
Shigenori Kabashima, Shigenori Kabashima, } "Strain and temperature monitoring in composite sandwich panels in space environment", Proc. SPIE 4185, Fourteenth International Conference on Optical Fiber Sensors, 41851C (9 November 2000); doi: 10.1117/12.2302191; https://doi.org/10.1117/12.2302191
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