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F-15 composite engine access doorThis paper presents a summary of the successfully concluded phase 1 of the two-phase Design and Manufacture of Advanced Thermoplastic Structures (DMATS) program. It addresses the design, manufacture, and validation testing of a thermoplastic F-15E forward engine access door and includes lessons learned during the concurrent product and process design development phases of the program.
Document ID
19930021253
Acquisition Source
Legacy CDMS
Document Type
Conference Paper
Authors
Ramkumar, Ramaswamy L. (Northrop Corp. Hawthorne, CA, United States)
Watson, James C. (McDonnell Aircraft Co. Saint Louis, MO., United States)
Date Acquired
September 6, 2013
Publication Date
January 1, 1991
Publication Information
Publication: NASA. Langley Research Center, The First NASA Advanced Composites Technology Conference, Part 1
Subject Category
Composite Materials
Accession Number
93N30442
Funding Number(s)
CONTRACT_GRANT: F33615-87-C-5242
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.

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