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Design, process development, manufacture, test and evaluation of boron-aluminum for space shuttle components
| Content Provider | NASA Technical Reports Server (NTRS) |
|---|---|
| Author | Garrett, R. A. |
| Copyright Year | 1973 |
| Description | The development of sufficient technology to permit application of boron-aluminum to space shuttle components is described. Specifically, report is made of the fabrication and testing of a 48 in. by 72 in. boron-aluminum compression panel capable of distributing a point load of 350,000 lbs. into a uniform running load within a peaking factor of 1.3 at a temperature of 600 F. In addition, small component testing was performed to verify the compression panel design. |
| File Size | 13912854 |
| Page Count | 48 |
| File Format | |
| Alternate Webpage(s) | http://archive.org/details/NASA_NTRS_Archive_19730015146 |
| Archival Resource Key | ark:/13960/t8jd9n265 |
| Language | English |
| Publisher Date | 1973-03-10 |
| Access Restriction | Open |
| Subject Keyword | Space Vehicles High Temperature Tests Mechanical Properties Aluminum Alloys Load Distribution Forces Boron Alloys Space Shuttles 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 |
