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Wide temperature range fiber optic cable: Cable design studyFactors considered in the design and fabrication of a single fiber optic cable intended for spacecraft applications in an environment of temperature extremes from -160 C to 125 C include: abrasion resistance, low temperature flexibility, small size, low weight, and overall temperature stability. Specific requirements were identified for fiber core and overall diameters, fiber loss and NA, and cable tensile load. The single fiber cable will be fabricated by using a chemical vapor step index fiber of .125 mm coated to .3 mm with RTV silicone and then extruded with a jacket of Teflon PFA to a diameter of .5 mm. Six yarns of 1420 denier unimpregnated Kevlar 49 with a helical lay of 1.3 inches will surround the jacketed fiber under an extrusion of PFA. The finished cable diameter will measure 1.8 mm, and the weight of one kilometer length will be approximately 4350grams.
Document ID
19780016981
Acquisition Source
Legacy CDMS
Document Type
Contractor Report (CR)
Authors
Speed, E. U.
(ITT Electro-Optical Products Div. Roanoke, VA, United States)
Date Acquired
August 9, 2013
Publication Date
January 1, 1978
Subject Category
Optics
Report/Patent Number
NASA-CR-157061
Report Number: NASA-CR-157061
Accession Number
78N24924
Funding Number(s)
CONTRACT_GRANT: JPL-954843
CONTRACT_GRANT: NAS7-100
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.
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