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Thermophysical properties data on graphite/polyimide composite materialsExperimental data for the thermal conductivity, thermal expansion, specific heat, and emittance of laminates of HTS/NR 150B2 and HTS/PMR 15 are presented. Measurements were made over the temperature range 116 K to 588 K. Results for the two materials were similar with some differences attributable to laminate quality. Higher expansion coefficients for the HTS/PMR 15 specimens in the resin-dominated directions indicate a higher coefficient for PMR 15 than NR 150B2.
Document ID
19800005940
Acquisition Source
Legacy CDMS
Document Type
Contractor Report (CR)
Authors
Campbell, M. D.
(General Dynamics/Convair San Diego, CA, United States)
Burleigh, D. D.
(General Dynamics/Convair San Diego, CA, United States)
Date Acquired
September 4, 2013
Publication Date
November 1, 1979
Subject Category
Composite Materials
Report/Patent Number
GDC-NAS-79-002
NASA-CR-159164
Report Number: GDC-NAS-79-002
Report Number: NASA-CR-159164
Accession Number
80N14197
Funding Number(s)
CONTRACT_GRANT: NAS1-15103
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.
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