Development of Parametric Mass and Volume Models for an Aerospace SOFC/Gas Turbine Hybrid System

In aerospace power systems, mass and volume are key considerations to produce a viable design. The utilization of fuel cells is being studied for a commercial aircraft electrical power unit. Based on preliminary analyses, a SOFC/gas turbine system may be a potential solution. This paper describes th...

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Bibliographische Detailangaben

Hauptverfasser:	Tornabene, Robert, Wang, Xiao-yen, Steffen, Christopher J., Jr, Freeh, Joshua E.
Format:	Report
Sprache:	eng
Schlagworte:	Aircraft Propulsion And Power
Online-Zugang:	Volltext bestellen
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