NASA Logo

NTRS

NTRS - NASA Technical Reports Server

Collections About News Help Login
Back to Results
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
Acquisition Source
Armstrong Flight Research Center
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
Meeting: AIAA/SAE/ASEE Joint Propulsion Conference
Location: Salt Lake City, UT
Country: United States
Start Date: July 25, 2016
End Date: July 27, 2016
Sponsors: American Inst. of Aeronautics and Astronautics, American Society for Electrical Engineers, Society of Automotive Engineers, Inc.
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.
Keywords
Hybrid Electric
distributed
propulsion

Related Records

IDRelationTitle20160009765See AlsoDesign and Development of a 200-kW Turbo-Electric Distributed Propulsion Testbed20170001279See AlsoDesign and Development of a 200-kW Turbo-Electric Distributed Propulsion Testbed
No Preview Available