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Massachusetts Institute of Technology
Types of turbomachinery best suited for space missions requiring power outputs in the range of few Kw to 1 Mw
Abstract
dc:descriptionThesis (M.S.)--Massachusetts Institute of Technology, Dept. of Aeronautics and Astronautics, 1988.
Degree
thesis:*- Department dc:contributor.department
- Massachusetts Institute of Technology. Dept. of Aeronautics and Astronautics.
- Grantor dc:publisher
- Massachusetts Institute of Technology
- Year dc:date.issued
- 1988
Author and committee
dc:creator, dc:contributor.*- Author dc:creator
-
- Benguedouar, Ammar
- Advisor dc:contributor.advisor
-
- Jean F. Louis.
Subjects
dc:subject × 1Rights
dc:rights- Statement 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.
- Licence dc:rights.uri
- Language dc:language.iso
- eng
Identifiers
dc:identifier.*- Handle dc:identifier.uri
- http://hdl.handle.net/1721.1/35933
- OAI identifier oai:identifier
- oai:dspace.mit.edu:1721.1/35933