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X-57 Cruise Motor and High-Lift Motor Mission Profile Power AnalysisThe X-57 Mission Profile Power Analysis was developed to evaluate the X-57 traction battery’s performance against Mod II, Mod III and Mod IV generic flight mission profiles. Traction battery system performance acceptance testing requirements were developed using data generated by this analysis. This analysis was also used to define the maximum power requirements for the traction system components.
Document ID
20230015689
Acquisition Source
Langley Research Center
Document Type
Other - Power Analysis
External Source(s)
https://www.nasa.gov/directorates/armd/x-57-technical-papers/#section-1
Authors
Keith Harris (Langley Research Center Hampton, Virginia, United States)
Date Acquired
October 31, 2023
Publication Date
April 12, 2021
Publication Information
Subject Category
Aircraft Design, Testing and Performance
Report/Patent Number
ANLYS-CEPT-018/Rev. D
Funding Number(s)
WBS: 107210.02.06.07
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.
Technical Review
NASA Peer Committee

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