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Hybrid FOSS Project

Metadata Updated: December 6, 2023

<p>Armstrong researchers are continuing their efforts to further develop FOSS technologies. A hybrid FOSS technique (HyFOSS) employs conventional continuous grating fibers and then overlays sections every 3-4 feet with &ldquo;strong&rdquo; gratings that can be sampled at higher rates. The new and stronger gratings can be sampled at rates up to 5,000 Hertz (Hz) while the continuous grating sections continue to be sampled at the lower 100 Hz rate. This technique enables higher spatial resolution at specific targets without sacrificing resolution in other areas. The ultimate goal is to achieve sampling rates up to 20 kHz.</p><p><strong>Work to date</strong>: The team began investigating the technique in early 2013 after a request from NASA Kennedy Space Center. Many aerospace and space vehicles &ndash; fighter aircraft, UAVs, launch vehicles, and spacecraft &ndash; could benefit from FOSS integration. Some of the applications require higher sample rates to maintain high spatial resolution. NASA Kennedy&rsquo;s Launch Services Group requested that the NASA Armstrong Advanced Structures and Measurements Group investigate the development effort that would be required to increase the sample rate from 100 hertz (Hz) to over 20 kHz. This increased sampling capability would allow structural features related to high frequency shock and/or vibration to be captured. To date, the OFDR technology does not have the capability to achieve these higher sample rates, though the possibility of fusing Wavelength Division Multiplexing (WDM) is feasible yet with limited spatial resolution. To achieve this with existing instrumentation would require the installation of two technologies, one utilizing OFDR and the other using WDM, and would increase the weight and installation requirement of fiber optic instrumentation.</p><p>Combining the best of OFDR and WDM technologies into new hardware that utilizes the same optical fiber would allow for high spatial resolution with lower sample rates in addition to the ability to obtain high sample rates at strategically spaced points along the fiber. With this goal, the hybrid FOSS (hyFOSS) system was developed.</p><p>A series of weak and strong FBGs are written onto the optical fiber. Weak FBGs allow for spatial resolution of 0.25 inches. The maximum number of stronger, unique-wavelength FBGs and the minimum separation interval between the sensors are determined by the length of the fiber and the wavelength spectrum of the light source. However, there is latitude to allow for the number and placement of the sensors to be tailored to the testing application.</p><p><strong>Looking ahead</strong>: Researchers have asked the company that currently provides the fibers to supply a 40-ft strand embedded with the new technology. Next steps involving investigating the specimen in the laboratory environment. The Armstrong team is also investigating the possibilities of pushing the overall sample rate to 20kHz.</p><p><strong><em>Benefits</em></strong></p><ul><li><strong>More measurements</strong>: Offers higher sampling rates (up to 5,000 Hz) for specific portions of the fiber</li><li><strong>Fast processing</strong>: Data can be collected at different resolutions enabling high resolution without sacrificing speed</li></ul><p><strong><em>Applications</em></strong></p><ul><li>Aeronautics and launch vehicles</li></ul>

Access & Use Information

Public: This dataset is intended for public access and use. License: No license information was provided. If this work was prepared by an officer or employee of the United States government as part of that person's official duties it is considered a U.S. Government Work.

Downloads & Resources

References

http://techport.nasa.gov/home
http://techport.nasa.gov/doc/home/TechPort_Advanced_Search.pdf
http://techport.nasa.gov/fetchFile?objectId=6561
http://techport.nasa.gov/fetchFile?objectId=3456
http://techport.nasa.gov/fetchFile?objectId=3447
http://techport.nasa.gov/fetchFile?objectId=6584
http://techport.nasa.gov/fetchFile?objectId=6560
http://techport.nasa.gov/fetchFile?objectId=3448

Dates

Metadata Created Date November 12, 2020
Metadata Updated Date December 6, 2023

Metadata Source

Harvested from NASA Data.json

Additional Metadata

Resource Type Dataset
Metadata Created Date November 12, 2020
Metadata Updated Date December 6, 2023
Publisher Human Exploration and Operations Mission Directorate
Maintainer
Identifier TECHPORT_14675
Data First Published 2013-01-01
Data Last Modified 2020-01-29
Public Access Level public
Bureau Code 026:00
Metadata Context https://project-open-data.cio.gov/v1.1/schema/catalog.jsonld
Metadata Catalog ID https://data.nasa.gov/data.json
Schema Version https://project-open-data.cio.gov/v1.1/schema
Catalog Describedby https://project-open-data.cio.gov/v1.1/schema/catalog.json
Harvest Object Id 875c593a-50f6-4364-9b06-426c863e00df
Harvest Source Id 58f92550-7a01-4f00-b1b2-8dc953bd598f
Harvest Source Title NASA Data.json
Homepage URL http://techport.nasa.gov/view/14675
Program Code 026:000
Related Documents http://techport.nasa.gov/home, http://techport.nasa.gov/doc/home/TechPort_Advanced_Search.pdf, http://techport.nasa.gov/fetchFile?objectId=6561, http://techport.nasa.gov/fetchFile?objectId=3456, http://techport.nasa.gov/fetchFile?objectId=3447, http://techport.nasa.gov/fetchFile?objectId=6584, http://techport.nasa.gov/fetchFile?objectId=6560, http://techport.nasa.gov/fetchFile?objectId=3448
Source Datajson Identifier True
Source Hash b8119af900ecd03be26f6d28b1203f4ca839b56bb1dd9e4dc847a0816dee8400
Source Schema Version 1.1

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