| dc.contributor.advisor | Richard H. Battin. | en_US |
| dc.contributor.author | Dierlam, Todd Allen | en_US |
| dc.date.accessioned | 2008-09-03T15:49:22Z | |
| dc.date.available | 2008-09-03T15:49:22Z | |
| dc.date.copyright | 1990 | en_US |
| dc.date.issued | 1990 | en_US |
| dc.identifier.uri | http://hdl.handle.net/1721.1/42490 | |
| dc.description | Thesis (M.S.)--Massachusetts Institute of Technology, Dept. of Aeronautics and Astronautics, 1990. | en_US |
| dc.description | Includes bibliographical references (leaves 167-168). | en_US |
| dc.description.statementofresponsibility | by Todd Allen Dierlam. | en_US |
| dc.format.extent | 168 leaves | en_US |
| 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 | en_US |
| dc.subject | Aeronautics and Astronautics | en_US |
| dc.title | Entry vehicle performance analysis and atmospheric guidance algorithm for precision landing on Mars | 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 | 25315321 | en_US |
