| dc.contributor.advisor | Jean F. Louis. | en_US |
| dc.contributor.author | Benguedouar, Ammar | en_US |
| dc.contributor.other | Massachusetts Institute of Technology. Dept. of Aeronautics and Astronautics. | en_US |
| dc.date.accessioned | 2007-02-21T10:02:15Z | |
| dc.date.available | 2007-02-21T10:02:15Z | |
| dc.date.copyright | 1988 | en_US |
| dc.date.issued | 1988 | en_US |
| dc.identifier.uri | http://hdl.handle.net/1721.1/35933 | |
| dc.description | Thesis (M.S.)--Massachusetts Institute of Technology, Dept. of Aeronautics and Astronautics, 1988. | en_US |
| dc.description | Bibliography: leaves 96-103. | en_US |
| dc.description.statementofresponsibility | by Ammar Benguedouar. | en_US |
| dc.format.extent | 103 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 | |
| dc.subject | Aeronautics and Astronautics. | en_US |
| dc.title | Types of turbomachinery best suited for space missions requiring power outputs in the range of few Kw to 1 Mw | 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 | 18367445 | en_US |
