3 June 1987 Rf Fiber Optic Links For Spacecraft And Aircraft Applications
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Proceedings Volume 0756, Optical Technologies for Space Communication Systems; (1987) https://doi.org/10.1117/12.940035
Event: OE LASE'87 and EO Imaging Symposium, 1987, Los Angeles, CA, United States
For many spacecraft and avionic applications, weight, size and layout flexibility are critical parameters for transmission media. This paper describes the advantages of using RF fiber optic links as replacements for waveguides and coaxial cable, and describes the measured performance of a 2.85 to 3.15 GHz link and a widehand 2 to 12 GHz link.
© (1987) COPYRIGHT Society of Photo-Optical Instrumentation Engineers (SPIE). Downloading of the abstract is permitted for personal use only.
W. M. Bruno, W. E. Stephens, and T. R. Joseph "Rf Fiber Optic Links For Spacecraft And Aircraft Applications", Proc. SPIE 0756, Optical Technologies for Space Communication Systems, (3 June 1987); doi: 10.1117/12.940035; https://doi.org/10.1117/12.940035


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