Accession Number : ADA303117
Title : Development of LARC 160/NR150B2 Polyimide Graphite Hybrid Composites,
Corporate Author : SRI INTERNATIONAL MENLO PARK CA
Personal Author(s) : Maximovich, M. G. ; Bergren, O. ; Lockerby, S.
PDF Url : ADA303117
Report Date : MAR 1980
Pagination or Media Count : 62
Abstract : Because graphite-polyimide composite materials exhibit high performance, low weight, and good thermal-oxidative stability, they are promising candidates for space shuttle applications. Materials that are being evaluated all have serious shortcomings. No single material is rated excellent in all important respects: processibility, thermal oxidative stability at 316 deg C, toughness, and mechanical properties. The objectives of this project were (1) to develop and optimize a method for co-curing NR150B2 and LARC 160 prepregs into hybrid composites and (2) to evaluate and compare the processing characteristics and the properties of the hybrid composites with those of laminates fabricated from the individual component prepregs. jg p3
Descriptors : *COMPOSITE MATERIALS, *GRAPHITE, *HYBRID SYSTEMS, *POLYIMIDE PLASTICS, MECHANICAL PROPERTIES, SPACE TECHNOLOGY, MATERIALS, PROCESSING, LAMINATES, THERMAL STABILITY, TOUGHNESS, OXIDATION, SPACE SHUTTLES, LIGHTWEIGHT, PREPREGS.
Subject Categories : Laminates and Composite Materials
Distribution Statement : APPROVED FOR PUBLIC RELEASE