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Advanced composite structural concepts and materials technologies for primary aircraft structures: Advanced material conceptsTo achieve acceptable performance and long-term durability at elevated temperatures (350 to 600 F) for high-speed transport systems, further improvements of the high-performance matrix materials will be necessary to achieve very long-term (60,000-120,000 service hours) retention of mechanical properties and damage tolerance. This report emphasizes isoimide modification as a complementary technique to semi-interpenetrating polymer networks (SIPN's) to achieve greater processibility, better curing dynamics, and possibly enhanced thermo-mechanical properties in composites. A key result is the demonstration of enhanced processibility of isoimide-modified linear and thermo-setting polyimide systems.
Document ID
19950022606
Acquisition Source
Legacy CDMS
Document Type
Contractor Report (CR)
Authors
Lau, Kreisler S. Y.
(Lockheed Missiles and Space Co. Palo Alto, CA., United States)
Landis, Abraham L.
(Lockheed Missiles and Space Co. Palo Alto, CA., United States)
Chow, Andrea W.
(Lockheed Missiles and Space Co. Palo Alto, CA., United States)
Hamlin, Richard D.
(Lockheed Missiles and Space Co. Palo Alto, CA., United States)
Date Acquired
September 6, 2013
Publication Date
February 1, 1993
Subject Category
Aircraft Design, Testing And Performance
Report/Patent Number
NAS 1.26:4485
NASA-CR-4485
Report Number: NAS 1.26:4485
Report Number: NASA-CR-4485
Accession Number
95N29027
Funding Number(s)
CONTRACT_GRANT: NAS1-18888
PROJECT: RTOP 510-02-13-01
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.
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