NASA NTRS · 19920023278
Development of thermoplastic components for structural validation
Abstract
Recent activity directed toward advancing the development and validation of graphite reinforced thermoplastic primary and secondary structures is described. The efforts discussed include the design, manufacture and test of a highly-loaded multi-spar wing-box component, and the development of a flight-worthy article that is form, fit and functionally replaceable with the nose landing gear door of the V-22 Osprey.
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Avery, John G., Cassatt, Gary G.. 1990-09-01. Development of thermoplastic components for structural validation. https://ntrs.nasa.gov/citations/19920023278
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