| dc.contributor.advisor | Richard H. Battin, Gilbert S. Stubbs. | en_US |
| dc.contributor.author | Corvin, Michael Alexander | en_US |
| dc.contributor.other | Massachusetts Institute of Technology. Dept. of Aeronautics and Astronautics. | en_US |
| dc.date.accessioned | 2005-08-09T16:53:59Z | |
| dc.date.available | 2005-08-09T16:53:59Z | |
| dc.date.copyright | 1988 | en_US |
| dc.date.issued | 1988 | en_US |
| dc.identifier.uri | http://hdl.handle.net/1721.1/14371 | |
| dc.description | Thesis (M.S.)--Massachusetts Institute of Technology, Dept. of Aeronautics and Astronautics, 1988. | en_US |
| dc.description | Includes bibliographical references. | en_US |
| dc.description.statementofresponsibility | by Michael Alexander Corvin. | en_US |
| dc.format.extent | 108 p. | en_US |
| dc.format.extent | 7732524 bytes | |
| dc.format.extent | 7732286 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 | Ascent guidance for a winged boost vehicle | 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 | 20054837 | en_US |