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  5. Types of turbomachinery best suited for space missions requiring power outputs in the range of few Kw to 1 Mw

Types of turbomachinery best suited for space missions requiring power outputs in the range of few Kw to 1 Mw

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Author(s)
Benguedouar, Ammar
Advisor(s)
Jean F. Louis.
Date Issued
1988
Publisher
Massachusetts Institute of Technology
Description
Thesis (M.S.)--Massachusetts Institute of Technology, Dept. of Aeronautics and Astronautics, 1988.
Bibliography: leaves 96-103.
Subjects
Aeronautics and Astronautics.
MIT Department
Massachusetts Institute of Technology. Department of Aeronautics and Astronautics
Terms of Use
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.
http://dspace.mit.edu/handle/1721.1/7582
Persistent DSpace Link
http://hdl.handle.net/1721.1/35933
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