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Fiberoptics for liquid propellant rocket engine environmentsInterest is increasing in the use of fiberoptics on liquid-fueled rocket engines in recognition of their immunity to lightning and EMI, light weight, high-frequency response, and the possibility offered by optical technologies to measure additional important engine parameters for which present measurement methods are impractical. This paper discusses the requirements to be placed on fiberoptics applied to liquid-fueled rocket engines; identifies manufacturers of fibers that appear to have promise for the harsh rocket engine applications; and summarizes information on the characteristics of these fibers obtained from the manufacturers, program testing, and the general literature.
Document ID
19890059441
Acquisition Source
Legacy CDMS
Document Type
Conference Paper
Authors
Delcher, R.
(Rockwell International Corp. Canoga Park, CA, United States)
Dergevorkian, A.
(Rockwell International Corp. Canoga Park, CA, United States)
Barkhoudarian, S.
(Rockwell International Corp. Rocketdyne Div., Canoga Park, CA, United States)
Date Acquired
August 14, 2013
Publication Date
July 1, 1989
Subject Category
Optics
Report/Patent Number
AIAA PAPER 89-2416
Report Number: AIAA PAPER 89-2416
Accession Number
89A46812
Funding Number(s)
CONTRACT_GRANT: NAS3-25346
Distribution Limits
Public
Copyright
Other

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