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

Author(s)
Benguedouar, Ammar
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Massachusetts Institute of Technology. Dept. of Aeronautics and Astronautics.
Advisor
Jean F. Louis.
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Description
Thesis (M.S.)--Massachusetts Institute of Technology, Dept. of Aeronautics and Astronautics, 1988.
 
Bibliography: leaves 96-103.
 
Date issued
1988
URI
http://hdl.handle.net/1721.1/35933
Department
Massachusetts Institute of Technology. Department of Aeronautics and Astronautics
Publisher
Massachusetts Institute of Technology
Keywords
Aeronautics and Astronautics.
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