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Design and Development of a 200-kw Turbo-Electric Distributed Propulsion TestbedThis test bench represents a significant risk mitigation for creating the turbo-electric flying demonstrator.
Document ID
20160009766
Document Type
Presentation
Authors
Papathakis, Kurt V. (NASA Armstrong Flight Research Center Edwards, CA, United States)
Kloesel, Kurt J. (NASA Armstrong Flight Research Center Edwards, CA, United States)
Lin, Yohan (NASA Armstrong Flight Research Center Edwards, CA, United States)
Clarke, Sean (NASA Armstrong Flight Research Center Edwards, CA, United States)
Ediger, Jacob J. (NASA Armstrong Flight Research Center Edwards, CA, United States)
Ginn, Starr (NASA Armstrong Flight Research Center Edwards, CA, United States)
Date Acquired
August 2, 2016
Publication Date
July 25, 2016
Subject Category
Aircraft Propulsion and Power
Electronics and Electrical Engineering
Report/Patent Number
AFRC-E-DAA-TN33325
Meeting Information
AIAA/SAE/ASEE Joint Propulsion Conference(Salt Lake City, UT)
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.
Keywords
Hybrid Electric
distributed
propulsion

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