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Optimization of aircraft interior panels
| Content Provider | NASA Technical Reports Server (NTRS) |
|---|---|
| Author | Kourtides, Demetrius A. Roper, Willard D. |
| Copyright Year | 1986 |
| Description | Eight different graphite composite panels were fabricated using four different resin matrices. The resin matrices included Hercules 71775, a blend of vinylpolystyrpyridine and bismaleimide, H795, a bismaleimide, Cycom 6162, a phenolic, and PSP 6022M, a polystyrylpyridine. Graphite panels were fabricated using fabric or unidirectional tape. This report describes the processes for preparing these panels and some of their mechanical, thermal and flammability properties. Panel properties are compared with state-of-the-art epoxy fiberglass composite panels. |
| File Size | 2902414 |
| Page Count | 44 |
| File Format | |
| Alternate Webpage(s) | http://archive.org/details/NASA_NTRS_Archive_19870009114 |
| Archival Resource Key | ark:/13960/t4fn62b3h |
| Language | English |
| Publisher Date | 1986-07-01 |
| Access Restriction | Open |
| Subject Keyword | Air Transportation And Safety Panels Epoxy Matrix Composites Graphite Flammability Mechanical Properties Composite Structures Aircraft Structures Resin Matrix Composites Optimization Glass Fibers Bismaleimide Ntrs Nasa Technical Reports Server (ntrs) Nasa Technical Reports Server Aerodynamics Aircraft Aerospace Engineering Aerospace Aeronautic Space Science |
| Content Type | Text |
| Resource Type | Technical Report |
