NASA Logo

NTRS

NTRS - NASA Technical Reports Server

Back to Results
High molecular weight first generation PMR polyimides for 343 C applicationsThe effect of molecular weight on 343 C thermo-oxidative stability (TOS), mechanical properties, and processability, of the first generation PMR polyimides was studied. Graphite fiber reinforced PMR-15, PMR-30, PMR-50, and PMR-75 composites (corresponding to formulated molecular weights of 1500, 3000, 5000, and 7500, respectively) were fabricated using a simulated autoclave process. The data reveal that while alternate autoclave cure schedules are required for the high molecular weight resins, low void laminates can be fabricated which have significantly improved TDS over PMR-15, with only a small sacrifice in mechanical properties.
Document ID
19920067195
Acquisition Source
Legacy CDMS
Document Type
Reprint (Version printed in journal)
Authors
Malarik, D. C.
(NASA Lewis Research Center Cleveland, OH, United States)
Vannucci, R. D.
(NASA Lewis Research Center Cleveland, OH, United States)
Date Acquired
August 15, 2013
Publication Date
July 1, 1992
Publication Information
Publication: SAMPE Quarterly
Volume: 23
Issue: 4, Ju
ISSN: 0036-0821
Subject Category
Composite Materials
Accession Number
92A49819
Distribution Limits
Public
Copyright
Other

Available Downloads

There are no available downloads for this record.
No Preview Available