9 November 2000 Optical fiber sensors for spacecraft applications
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Proceedings Volume 4185, Fourteenth International Conference on Optical Fiber Sensors; 418559 (2000) https://doi.org/10.1117/12.2302332
Event: Fourteenth International Conference on Optical Fiber Sensors, 2000, Venice, Italy
Abstract
The significant advantages of optical fiber sensor systems for spacecraft applications have been established through demonstration projects on both prototype exemplars and flight articles. These include distributed strain sensing using embedded and surface-mounted fiber Bragg grating arrays and ultrahigh sensitivity strain and temperature sensing with fiber cavity etalon sensors. These projects will be discussed with emphasis on sensor performance, reliability, and survivability during composite fabrication, including egress of the fiber lead from the part.
© (2000) COPYRIGHT Society of Photo-Optical Instrumentation Engineers (SPIE). Downloading of the abstract is permitted for personal use only.
E. Joseph Friebele, E. Joseph Friebele, } "Optical fiber sensors for spacecraft applications", Proc. SPIE 4185, Fourteenth International Conference on Optical Fiber Sensors, 418559 (9 November 2000); doi: 10.1117/12.2302332; https://doi.org/10.1117/12.2302332
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