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The Langley turbo-prop commuter design: A complete project descriptionThe primary objective of this project was to propose and prove the possibility of a new, advanced technology commuter aircraft design. Among the specifications were short to medium range capabilities, low seat per mile cost, fuel efficiency, and passenger comfort. Based on market evaluation, we found that the optimum size for new regional aircraft is around 50 passengers; we have designed our aircraft for this capacity. Turboprop engines provide substantial reductions in operating costs due to lower fuel consumption. We have therefore chosen an advanced turboprop engine. Composite materials, while more expensive to purchase and manufacture, result in decreased costs later through weight savings and ease of replacement.
Document ID
19920012297
Acquisition Source
Legacy CDMS
Document Type
Contractor Report (CR)
Authors
Buttram, Greg
(Auburn Univ. AL, United States)
Horton, Keith
(Auburn Univ. AL, United States)
Keeter, Tim
(Auburn Univ. AL, United States)
Millhouse, Paul
(Auburn Univ. AL, United States)
Newberry, Kelli
(Auburn Univ. AL, United States)
Obyrne, Brian
(Auburn Univ. AL, United States)
Date Acquired
September 6, 2013
Publication Date
June 4, 1991
Subject Category
Aircraft Design, Testing And Performance
Report/Patent Number
NAS 1.26:189987
NASA-CR-189987
Report Number: NAS 1.26:189987
Report Number: NASA-CR-189987
Accession Number
92N21540
Funding Number(s)
CONTRACT_GRANT: NASW-4435
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.
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