dc.contributor.advisor | Walter M. Hollister. | en_US |
dc.contributor.author | Russ, David Phillip | en_US |
dc.contributor.other | Massachusetts Institute of Technology. Dept. of Aeronautics and Astronautics. | en_US |
dc.date.accessioned | 2007-01-10T15:50:55Z | |
dc.date.available | 2007-01-10T15:50:55Z | |
dc.date.copyright | 1988 | en_US |
dc.date.issued | 1988 | en_US |
dc.identifier.uri | http://hdl.handle.net/1721.1/35340 | |
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 David Phillip Russ. | en_US |
dc.format.extent | 70 leaves | en_US |
dc.format.extent | 2523039 bytes | |
dc.format.extent | 2695403 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 | Analysis of a heavy lift launch vehicle design using small liquid rocket engines | 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 | 19283930 | en_US |