Accession Number : ADA302703
Title : Design Allowables Test Program, Celion 3OOO/PMR-l5 and Celion 6000/PMR-l5 Graphite/Polyimide Composites.
Descriptive Note : Final contractor rept.,
Corporate Author : BOEING AEROSPACE CO SEATTLE WA ENGINEERING TECHNOLOGY DIV
Personal Author(s) : Cushman, J. B. ; McCleskey, S. F.
PDF Url : ADA302703
Report Date : JUN 1982
Pagination or Media Count : 210
Abstract : A design allowables test program was conducted on Celion 3000/PMR-l5 and Celion 6000/PMR-15 graphite/polyimide composite to establish material performance over a 116K (-250 deg F) to 589K (600 deg F) temperature range. Effects of aging, thermal cycling and moisture were also evaluated. Tension, compression and 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. (MM)
Descriptors : *LAMINATES, *FIBER REINFORCED COMPOSITES, *GRAPHITE, *AEROSPACE CRAFT, *POLYIMIDE PLASTICS, COMPRESSION, AGING(MATERIALS), STIFFNESS, THERMAL EXPANSION, BONDED JOINTS, SHEAR STRESSES, DESIGN CRITERIA, FAILURE(MECHANICS), CYCLIC LOADS, MICROCRACKING, BOLTED JOINTS.
Subject Categories : Research and Experimental Aircraft
Laminates and Composite Materials
Distribution Statement : APPROVED FOR PUBLIC RELEASE