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Fiberoptic characteristics for extreme operating environmentsFiberoptics could offer several major benefits for cryogenic liquid-fueled rocket engines, including lightning immunity, weight reduction, and the possibility of implementing a number of new measurements for engine condition monitoring. The technical feasibility of using fiberoptics in the severe environments posed by cryogenic liquid-fueled rocket engines was determined. The issues of importance and subsequent requirements for this use of fiberoptics were compiled. These included temperature ranges, moisture embrittlement succeptability, and the ability to withstand extreme shock and vibration levels. Different types of optical fibers were evaluated and several types of optical fibers' ability to withstand use in cryogenic liquid-fueled rocket engines was demonstrated through environmental testing of samples. This testing included: cold-bend testing, moisture embrittlement testing, temperature cycling, temperature extremes testing, vibration testing, and shock testing. Three of five fiber samples withstood the tests to a level proving feasibility, and two of these remained intact in all six of the tests. A fiberoptic bundle was also tested, and completed testing without breakage. Preliminary cabling and harnessing for fiber protection was also demonstrated. According to cable manufacturers, the successful -300 F cold bend, vibration, and shock tests are the first instance of any major fiberoptic cable testing below roughly -55 F. This program has demonstrated the basic technical feasibility of implementing optical fibers on cryogenic liquid-fueled rocket engines, and a development plan is included highlighting requirements and issues for such an implementation.
Document ID
19930010460
Acquisition Source
Legacy CDMS
Document Type
Contractor Report (CR)
Authors
Delcher, R. C.
(Rockwell International Corp. Canoga Park, CA, United States)
Date Acquired
September 6, 2013
Publication Date
May 29, 1992
Subject Category
Spacecraft Propulsion And Power
Report/Patent Number
RI/RD90-115
NASA-CR-189189
NAS 1.26:189189
Report Number: RI/RD90-115
Report Number: NASA-CR-189189
Report Number: NAS 1.26:189189
Accession Number
93N19649
Funding Number(s)
CONTRACT_GRANT: NAS3-25346
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.
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