NASA Logo

NTRS

NTRS - NASA Technical Reports Server

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

Back to Results
Large-diameter carbon-composite monofilamentsLarge-diameter carbon composite monofilaments with high strength and high modulus were produced by pregging multifiber carbon bundles with suitable organic resins and pyrolysing them together. Two approaches were developed to increase the utilization of fiber tensile strength by minimizing stress concentration defects induced by dissimilar shrinkage during pyrolysis. These were matrix modification to improve char yield and strain-to-failure and fiber-matrix copyrolysis to alleviate matrix cracking. Highest tensile strength and modulus were obtained by heat treatments to 2873 K to match fiber and matrix strain-to-failure and develop maximum monofilament tensile-strength and elastic modulus.
Document ID
19740018929
Acquisition Source
Legacy CDMS
Document Type
Contractor Report (CR)
Authors
Bradshaw, W. G.
(Lockheed Missiles and Space Co. Palo Alto, CA, United States)
Pinoli, P. C.
(Lockheed Missiles and Space Co. Palo Alto, CA, United States)
Karlak, R. F.
(Lockheed Missiles and Space Co. Palo Alto, CA, United States)
Date Acquired
September 3, 2013
Publication Date
May 1, 1974
Subject Category
Materials, Nonmetallic
Report/Patent Number
LMSC-D358951
NASA-CR-134625
Report Number: LMSC-D358951
Report Number: NASA-CR-134625
Accession Number
74N27042
Funding Number(s)
CONTRACT_GRANT: NAS3-16794
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.
No Preview Available