1 February 1991 Fiber optic temperature sensor for aerospace applications
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Proceedings Volume 1369, Fiber Optic Systems for Mobile Platforms IV; (1991); doi: 10.1117/12.24827
Event: SPIE Microelectronic Interconnect and Integrated Processing Symposium, 1990, San Jose, United States
Abstract
A fiber-optic temperature sensor has been developed for aerospace applications on the basis of the time rate of decay (TRD) principle, with a view to an operational temperature range of -60 to 350 C. This TRD system has completed qualification testing and will then undergo flight tests. Attention is presently given to the design and performance of four low temperature sensors that are subelements of the larger sensor system; in order to convert analog signals into over/under temperature indications, simple comparators are implemented in software.
© (1991) COPYRIGHT Society of Photo-Optical Instrumentation Engineers (SPIE). Downloading of the abstract is permitted for personal use only.
Stephen Charles Jensen, Shelle Dawn Tilstra, Geoffrey A. Barnabo, David C. Thomas, Richard W. Phillips, "Fiber optic temperature sensor for aerospace applications", Proc. SPIE 1369, Fiber Optic Systems for Mobile Platforms IV, (1 February 1991); doi: 10.1117/12.24827; https://doi.org/10.1117/12.24827
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