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Fiber Optic Temperature Sensors in TPS: Arc Jet Model Design & TestingTechniques for using fiber optics with Fiber Bragg Gratings (FBGs) have been developed by IFOS Corp. for use in thermal protection systems (TPS) on spacecraft heat shield materials through NASA Phase 1 and 2 SBIR efforts and have been further improved in a recent collaboration between IFOS and NASA that will be described here. Fiber optic temperature sensors offer several potential advantages over traditional thermocouple sensors including a) multiplexing many sensors in a single fiber to increase sensor density in a given array or to provide spatial resolution, b) improved thermal property match between sensor and TPS to reduce heat flow disruption, c) lack of electrical conductivity.
Document ID
20170010671
Acquisition Source
Ames Research Center
Document Type
Presentation
Authors
Black, Richard
(Intelligent Fiber-Optic Systems, Corp. Santa Clara, CA, United States)
Feldman, Jay
(NASA Ames Research Center Moffett Field, CA, United States)
Ellerby, Donald
(NASA Ames Research Center Moffett Field, CA, United States)
Monk, Joshua
(Analytical Mechanics Associates, Inc. Moffett Field, CA, United States)
Moslehi, Behzad
(Intelligent Fiber-Optic Systems, Corp. Santa Clara, CA, United States)
Oblea, Levy
(Intelligent Fiber-Optic Systems, Corp. Santa Clara, CA, United States)
Switzer, Matthew
(NASA Ames Research Center Moffett Field, CA, United States)
Date Acquired
November 7, 2017
Publication Date
June 26, 2017
Subject Category
Engineering (General)
Report/Patent Number
ARC-E-DAA-TN43529
Meeting Information
Meeting: National Space & Missile Materials Symposium (NSMMS)
Location: Indian Wells, CA
Country: United States
Start Date: June 26, 2017
End Date: June 29, 2017
Sponsors: National Space and Missiles Materials
Funding Number(s)
CONTRACT_GRANT: SAA2-40310
CONTRACT_GRANT: NNA15BB15C
Distribution Limits
Public
Copyright
Public Use Permitted.
Keywords
sensors
fiber optics
heat shield
TPS
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