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Intermediate Fidelity Closed Brayton Cycle Power Conversion ModelThis paper describes the implementation of an intermediate fidelity model of a closed Brayton Cycle power conversion system (Closed Cycle System Simulation). The simulation is developed within the Numerical Propulsion Simulation System architecture using component elements from earlier models. Of particular interest, and power, is the ability of this new simulation system to initiate a more detailed analysis of compressor and turbine components automatically and to incorporate the overall results into the general system simulation.
Document ID
20060024537
Acquisition Source
Glenn Research Center
Document Type
Technical Memorandum (TM)
Authors
Lavelle, Thomas M.
(NASA Glenn Research Center Cleveland, OH, United States)
Khandelwal, Suresh
(RS Information Systems, Inc. Cleveland, OH, United States)
Owen, Albert K.
(NASA Glenn Research Center Cleveland, OH, United States)
Date Acquired
August 23, 2013
Publication Date
March 1, 2006
Subject Category
Spacecraft Propulsion And Power
Report/Patent Number
NASA/TM-2006-213993
E-15317
Funding Number(s)
WBS: WBS 22-973-80-10
Distribution Limits
Public
Copyright
Public Use Permitted.
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