Loading...
Please wait, while we are loading the content...
Large boron--epoxy filament-wound pressure vessels
| Content Provider | NASA Technical Reports Server (NTRS) |
|---|---|
| Author | Jensen, W. M. Bailey, R. L. Knoell, A. C. |
| Copyright Year | 1973 |
| Description | Advanced composite material used to fabricate pressure vessel is prepeg (partially cured) consisting of continuous, parallel boron filaments in epoxy resin matrix arranged to form tape. To fabricate chamber, tape is wound on form which must be removable after composite has been cured. Configuration of boron--epoxy composite pressure vessel was determined by computer program. |
| File Size | 181324 |
| Page Count | 2 |
| File Format | |
| Alternate Webpage(s) | http://archive.org/details/NASA_NTRS_Archive_19730000038 |
| Archival Resource Key | ark:/13960/t7pp3vq2p |
| Language | English |
| Publisher Date | 1973-02-01 |
| Access Restriction | Open |
| Subject Keyword | Fabrication Technology Fabrication Boron Pressure Vessels Epoxy Resins Composite Wrapping Mathematical Models Filament Winding Computer Programs 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 |