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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. Previously announced in STAR as N80-14197
Document ID
19830051900
Acquisition Source
Legacy CDMS
Document Type
Conference Proceedings
Authors
Campbell, M. D.
(General Dynamics/Convair San Diego, CA, United States)
Burleigh, D. D.
(General Dynamics Corp. Convair Div., San Diego, CA, United States)
Date Acquired
August 11, 2013
Publication Date
January 1, 1982
Subject Category
Composite Materials
Accession Number
83A33118
Funding Number(s)
CONTRACT_GRANT: NAS1-15103
Distribution Limits
Public
Copyright
Other

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