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A six-wafer combustion system for a silicon micro gas turbine engine ...

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MEHRA et al.: 6-WAFER COMBUSTION SYSTEM FOR A SILICON MICRO GAS TURBINE ENGINE 527<br />

Christopher M. Spadaccini received the B.S. and<br />

M.S. degrees from the Department of Aeronautics<br />

and Astronautics, Massachusetts Institute of<br />

Technology (MIT), Cambridge, in 1997 and 1999,<br />

respectively. He is a graduate research assistant<br />

and is pursuing the Ph.D. degree with the MIT Gas<br />

Turbine Laboratory.<br />

His current research involves the development of<br />

a hydrocarbon-fueled <strong>micro</strong>scale <strong>combustion</strong> <strong>system</strong><br />

<strong>for</strong> a <strong>micro</strong> <strong>gas</strong> <strong>turbine</strong> <strong>engine</strong>. His research interests<br />

in the MEMS field include <strong>micro</strong>fluidics, <strong>combustion</strong> at the <strong>micro</strong>-scale, and<br />

high-speed <strong>micro</strong>-turbomachinery. Other areas of interest are aero-propulsion,<br />

fluid mechanics, reacting flows, thermodynamics and heat transfer, and shortduration<br />

turbomachinery testing.<br />

Mr. Spadaccini is a member of the American Society of Mechanical Engineers,<br />

the American Institute of Aeronautics and Astronautics, and the Sigma<br />

Xi National Research Society.

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