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Additional development of large diameter carbon monofilamentThe chemical vapor process for preparing a large diameter carbon-base monofilament from a BCl3, Ch4 and H2 gas mixture with a carbon substrate fiber was studied. The effect of reactor geometry, total gas flows and deposition temperature on the tensile strength of the monofilament were investigated. It was noted that consistent results could only be obtained when the carbon substrate fiber was cleaned. The strength of the monofilament was found to depend on the highest temperature and the temperature profile of the monofilament in the reactor. The strength of monofilament produced in the dc and RF reactors were found to be similar and similar alloy compositions in the monofilament were attained when the same gas ratios were used. The tensile strength of the monofilament at 500 C was found to be 60 to 70% of the room temperature tensile strength. No degradation was noted after exposure to molten aluminum.
Document ID
19740013052
Acquisition Source
Legacy CDMS
Document Type
Contractor Report (CR)
Authors
Jacob, B. A.
(United Aircraft Corp. East Hartford, CT, United States)
Veltri, R. D.
(United Aircraft Corp. East Hartford, CT, United States)
Date Acquired
September 3, 2013
Publication Date
February 1, 1974
Subject Category
Materials, Nonmetallic
Report/Patent Number
NASA-CR-134607
Report Number: NASA-CR-134607
Accession Number
74N21165
Funding Number(s)
CONTRACT_GRANT: NAS3-16803
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.
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