NASA Logo

NTRS

NTRS - NASA Technical Reports Server

Back to Results
Development of thermoplastic components for structural validationRecent 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.
Document ID
19920023278
Acquisition Source
Legacy CDMS
Document Type
Conference Paper
Authors
Avery, John G.
(Boeing Military Airplane Development Wichita, KS, United States)
Cassatt, Gary G.
(Boeing Military Airplane Development Wichita, KS, United States)
Date Acquired
September 6, 2013
Publication Date
September 1, 1990
Publication Information
Publication: NASA. Langley Research Center, Eighth DOD(NASA)FAA Conference on Fibrous Composites in Structural Design, Part 1
Subject Category
Composite Materials
Accession Number
92N32522
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.
Document Inquiry

Available Downloads

There are no available downloads for this record.
No Preview Available