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The all-electric aircraft - A systems view and proposed NASA research ProgramsIt is expected that all-electric aircraft, whether military or commercial, will exhibit reduced weight, acquisition cost and fuel consumption, an expanded flight envelope and improved survivability and reliability, simpler maintenance, and reduced support equipment. Also noteworthy are dramatic improvements in mission adaptability, based on the degree to which control system performance relies on easily exchanged software. Flight-critical secondary power and control systems whose malfunction would mean loss of an aircraft pose failure detection and design methodology problems, however, that have only begun to be addressed. NASA-sponsored research activities concerned with these problems and prospective benefits are presently discussed.
Document ID
19840054126
Acquisition Source
Legacy CDMS
Document Type
Reprint (Version printed in journal)
Authors
Spitzer, C. R.
(NASA Langley Research Center Hampton, VA, United States)
Date Acquired
August 12, 2013
Publication Date
May 1, 1984
Publication Information
Publication: IEEE Transactions on Aerospace and Electronic Systems
Volume: AES-20
ISSN: 0018-9251
Subject Category
Aircraft Propulsion And Power
Accession Number
84A36913
Distribution Limits
Public
Copyright
Other

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