NASA Logo

NTRS

NTRS - NASA Technical Reports Server

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

Back to Results
Research on graphite reinforced glass matrix compositesHigh levels of mechanical performance in tension, flexure, fatigue, and creep loading situations of graphite fiber reinforced glass matrix composites are discussed. At test temperatures of up to 813 K it was found that the major limiting factor was the oxidative instability of the reinforcing graphite fibers. Particular points to note include the following: (1) a wide variety of graphite fibers were found to be comparable with the glass matrix composite fabrication process; (2) choice of fiber, to a large extent, controlled resultant composite performance; (3) composite fatigue performance was found to be excellent at both 300 K and 703 K; (4) composite creep and stress rupture at temperatures of up to 813 K was limited by the oxidative stability of the fiber; (5) exceptionally low values of composite thermal expansion coefficient were attributable to the dimensional stability of both matrix and fiber; and (6) component fabricability was demonstrated through the hot pressing of hot sections and brazing using glass and metal joining phases.
Document ID
19800023932
Acquisition Source
Legacy CDMS
Document Type
Contractor Report (CR)
Authors
Prewo, K. M.
(United Technologies Research Center East Hartford, CT, United States)
Thompson, E. R.
(United Technologies Research Center East Hartford, CT, United States)
Date Acquired
September 4, 2013
Publication Date
February 1, 1980
Subject Category
Composite Materials
Report/Patent Number
NASA-CR-159312
R80-912545-49
Report Number: NASA-CR-159312
Report Number: R80-912545-49
Accession Number
80N32440
Funding Number(s)
CONTRACT_GRANT: NAS1-14346
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.
No Preview Available