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Development of lightweight graphite/polyimide sandwich panels, phases 3, 4 and 5
| Content Provider | NASA Technical Reports Server (NTRS) |
|---|---|
| Author | Merlette, J. B. |
| Copyright Year | 1972 |
| Description | Work performed in the last three phases of the program included: (1) face sheet processing; (2) honeycomb core manufacture; (3) face sheet-to-core bonding development; and (4) sandwich panel fabrication and testing. Resin cure studies were a major portion of this effort since processing problems traced to the polyimide matrix resin had to be resolved before quality core and face sheets could be fabricated. Honeycomb core fabrication and testing were conducted by Hexcel Corporation. A total of four graphite/polyimide resin composite cores were fabricated, tested, and reported. Two sandwich panels weighing .48 and .58 lb/sq ft, respectively were designed and fabricated which meet the support structure loads for the shuttle orbiter thermal protection system. |
| File Size | 4886074 |
| Page Count | 116 |
| File Format | |
| Alternate Webpage(s) | http://archive.org/details/NASA_NTRS_Archive_19730001776 |
| Archival Resource Key | ark:/13960/t15n10378 |
| Language | English |
| Publisher Date | 1972-10-01 |
| Access Restriction | Open |
| Subject Keyword | Machine Elements And Processes Structural Design Panels Composite Materials Honeycomb Cores Graphite Heat Shielding Manufacturing Space Shuttle Orbiters Sandwich Structures Polyimide Resins Ntrs Nasa Technical Reports ServerĀ (ntrs) Nasa Technical Reports Server Aerodynamics Aircraft Aerospace Engineering Aerospace Aeronautic Space Science |
| Content Type | Text |
| Resource Type | Technical Report |