Process development of silicon-silicon carbide hybrid structures for micro-engines (January 2002)
MEMS-based gas turbine engines are currently under development at MIT for use as a button-sized portable power generator or micro-aircraft propulsion sources. Power densities expected for the micro-engines require very high rotor peripheral speeds of 300-600m/s and high combustion gas temperatures o...
Main Authors: | , , |
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Format: | Article |
Language: | en_US |
Published: |
2003
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Subjects: | |
Online Access: | http://hdl.handle.net/1721.1/3983 |