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Fabrication process of a high temperature polymer matrix engine duct
| Content Provider | NASA Technical Reports Server (NTRS) |
|---|---|
| Author | Pratt, R. D. Wilson, A. J. |
| Copyright Year | 1985 |
| Description | The process that was used in the molding of an advanced composite outer by-pass duct planned for the F404 engine is discussed. This duct was developed as a potential replacement for the existing titanium duct in order to reduce both the weight and cost of the duct. The composite duct is now going into the manufacturing technology portion of the program. The duct is fabricated using graphite cloth impregnated with the PMR-15 matrix system. |
| File Size | 330397 |
| Page Count | 7 |
| File Format | |
| Alternate Webpage(s) | http://archive.org/details/NASA_NTRS_Archive_19860001823 |
| Archival Resource Key | ark:/13960/t3033qs0s |
| Language | English |
| Publisher Date | 1985-09-01 |
| Access Restriction | Open |
| Subject Keyword | Composite Materials Cost Effectiveness Weight Reduction Aircraft Construction Materials High Temperature Tests Fiber Composites Aircraft Design Aircraft Engines High Temperature Molding Materials Graphite-polyimide Composites Operating Temperature Air Ducts Ntrs Nasa Technical Reports Server (ntrs) Nasa Technical Reports Server Aerodynamics Aircraft Aerospace Engineering Aerospace Aeronautic Space Science |
| Content Type | Text |
| Resource Type | Article |
