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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
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