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)