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The document discusses reducing costs for composite aircraft structures from a materials perspective. It outlines that carbon fiber costs have decreased as the number of filaments per tow has increased, with developments up to 320,000 filaments per tow. Testing shows the mechanical properties of higher-filament count fibers are lower but still suitable. Epoxy matrix costs are driven by required service temperatures and complexity, though formulations curing under 100°C have been developed. Overall cost redu

Author

flqt9000

Language

EN