Preliminary weight and cost estimates have been prepared for design concepts utilized for a transonic long range transport airframe with extensive applications of advanced composite materials. The design concepts, manufacturing approach, and anticipated details of manufacturing cost reflected in the composite airframe are substantially different from those found in conventional metal structure and offer further evidence of the advantages of advanced composite materials.
Preliminary weight and cost estimates for transport aircraft composite structural design concepts
30.03.1973
Report
Keine Angabe
Englisch
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