Published June 1982
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Design Allowables Test program, Celion 3000/PMR-15 and Celion 6000/PMR-15, graphite/polyimide composites. Final Report
Description
A design allowables test program was conducted on Celion 3000/PRM-15 and Celion 6000/PMR-15 graphite/polyimide composite to establish material performance over a 116 K (-250 F) to 589 K (600 F) temperature range. Effects of aging, thermal cycling and moisture were also evaluated. Tension, compression and in plane shear properties were determined for uniaxial, pseudoisotropic and +45 laminates. Test results show sufficient strength and stiffness to substantiate graphite/polyimide composites as an acceptable structural material for high temperature structural applications
Availability note (English)
MF available from INIS under the Report Number; Available from NTIS, PC A10/MF A01.
Files
Additional details
Publishing Information
- Imprint Pagination
- 206 p.
- Report number
- N--8230338
INIS
- Country of Publication
- United States
- Country of Input or Organization
- United States
- INIS RN
- 14782942
- Subject category
- S36: MATERIALS SCIENCE;
- Descriptors DEI
- AGING; COMPOSITE MATERIALS; GRAPHITE; HUMIDITY; IMIDES; MATERIALS TESTING; MECHANICAL PROPERTIES; TEMPERATURE DEPENDENCE; THERMAL CYCLING; THERMAL FATIGUE
- Descriptors DEC
- CARBON; ELEMENTS; FATIGUE; MATERIALS; NONMETALS; ORGANIC COMPOUNDS; ORGANIC NITROGEN COMPOUNDS; TESTING
Optional Information
- Secondary number(s)
- NASA-CR--165840.