NASA NTRS · 19930021253
F-15 composite engine access door
Abstract
This 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.
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Ramkumar, Ramaswamy L., Watson, James C.. 1991-01-01. F-15 composite engine access door. https://ntrs.nasa.gov/citations/19930021253
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