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Validation of the NASA Electrical Power System – Sizing and Analysis Tool (EPS-SAT)The electrification of aircraft propulsion systems has opened the design space for engineers by allowing for unique and highly specialized propulsion system and vehicle designs. NASA developed the Electrical Power System – Sizing and Analysis Tool (EPS-SAT) to conduct high-level trade studies and sensitivity studies on the various propulsion system designs that can be implemented in electrified aircraft. The results of these studies would be used to better direct investment dollars and determine strengths and weaknesses of propulsion system designs. In this paper, the results of the EPS-SAT tool were validated with hardware data extracted from the NASA Revolutionary Vertical Lift Technology (RVLT) Advanced Reconfigurable Electric Aircraft Lab (AREAL). Updated performance maps were added to the EPS-SAT library so that high-fidelity results could be calculated.
Document ID
20240007900
Acquisition Source
Glenn Research Center
Document Type
Conference Paper
Authors
Patrick A. Hanlon
(Glenn Research Center Cleveland, United States)
Brian P. Malone
(Glenn Research Center Cleveland, United States)
David J. Sadey
(Glenn Research Center Cleveland, United States)
Keith R. Hunker
(Glenn Research Center Cleveland, United States)
Casey J. Theman
(Glenn Research Center Cleveland, United States)
Xavier Collazo-Fernandez
(Glenn Research Center Cleveland, United States)
Trey D. Rupp
(Glenn Research Center Cleveland, United States)
Paul M. Nowak
(Glenn Research Center Cleveland, United States)
Date Acquired
June 21, 2024
Subject Category
Aircraft Propulsion and Power
Meeting Information
Meeting: AIAA Aviation Forum and Exposition
Location: Las Vegas, NV
Country: US
Start Date: July 29, 2024
End Date: August 2, 2024
Sponsors: American Institute of Aeronautics and Astronautics
Funding Number(s)
WBS: 664817.02.03.02.01.02
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.
Technical Review
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