| dc.contributor.advisor | Paul A. Lagace. | en_US |
| dc.contributor.author | Williamson, James Edward | en_US |
| dc.date.accessioned | 2005-08-15T15:45:12Z | |
| dc.date.available | 2005-08-15T15:45:12Z | |
| dc.date.copyright | 1991 | en_US |
| dc.date.issued | 1991 | en_US |
| dc.identifier.uri | http://hdl.handle.net/1721.1/13040 | |
| dc.description | Thesis (M.S.)--Massachusetts Institute of Technology, Dept. of Aeronautics and Astronautics, 1991. | en_US |
| dc.description | Aero hard copy bound in 1 v. | en_US |
| dc.description | Includes bibliographical references. | en_US |
| dc.description.statementofresponsibility | by James Edward Williamson. | en_US |
| dc.format.extent | 2 v. (392 leaves) | en_US |
| dc.format.extent | 20724887 bytes | |
| dc.format.extent | 20724645 bytes | |
| dc.format.mimetype | application/pdf | |
| dc.format.mimetype | application/pdf | |
| dc.language.iso | eng | en_US |
| dc.publisher | Massachusetts Institute of Technology | en_US |
| dc.rights | M.I.T. theses are protected by copyright. They may be viewed from this source for any purpose, but reproduction or distribution in any format is prohibited without written permission. See provided URL for inquiries about permission. | en_US |
| dc.rights.uri | http://dspace.mit.edu/handle/1721.1/7582 | |
| dc.subject | Aeronautics and Astronautics | en_US |
| dc.title | Response mechanisms in the impact of graphite/epoxy honeycomb sandwich panels | en_US |
| dc.type | Thesis | en_US |
| dc.description.degree | M.S. | en_US |
| dc.contributor.department | Massachusetts Institute of Technology. Department of Aeronautics and Astronautics | |
| dc.identifier.oclc | 26164265 | en_US |
