Types of turbomachinery best suited for space missions requiring power outputs in the range of few Kw to 1 Mw
Thesis (M.S.)--Massachusetts Institute of Technology, Dept. of Aeronautics and Astronautics, 1988.
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| Формат: | Дисертація |
| Мова: | eng |
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Massachusetts Institute of Technology
2007
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| Онлайн доступ: | http://hdl.handle.net/1721.1/35933 |