NASA Logo

NTRS

NTRS - NASA Technical Reports Server

Press Enter or click the Search button to begin your search.

Back to Results
Determination of the durability of the fiberoptics in rocket engine environmentsThe results of a testing program in which selected optical fibers were exposed to extreme environments representative of those experienced on rocket engines are discussed. Included in the experiment are cold-bend testing, a moisture embrittlement test, a thermal cycling test, temperature extremes testing, vibration testing, and shock testing. Two of the fibers selected, the titanium-carbide-coated and the aluminum-jacketed silica samples succeeded in passing all the tests without a failure.
Document ID
19900055699
Acquisition Source
Legacy CDMS
Document Type
Conference Paper
Authors
Delcher, R.
(Rockwell International Corp. Canoga Park, CA, United States)
Dinnsen, D.
(Rockwell International Corp. Canoga Park, CA, United States)
Barkhoudarian, S.
(Rockwell International Corp. Canoga Park, CA, United States)
Cannon, I.
(Rockwell International Corp. Rocketdyne Div., Canoga Park, CA, United States)
Date Acquired
August 14, 2013
Publication Date
July 1, 1990
Subject Category
Optics
Report/Patent Number
AIAA PAPER 90-2229
Report Number: AIAA PAPER 90-2229
Accession Number
90A42754
Funding Number(s)
CONTRACT_GRANT: NAS3-25346
Distribution Limits
Public
Copyright
Other

Available Downloads

There are no available downloads for this record.
No Preview Available