NASA Logo

NTRS

NTRS - NASA Technical Reports Server

Back to Results
Fuel conservation merits of advanced turboprop transport aircraftThe advantages of a propfan powered aircraft for the commercial air transportation system were assessed by the comparison with an equivalent turbofan transport. Comparisons were accomplished on the basis of fuel utilization and operating costs, as well as aircraft weight and size. Advantages of the propfan aircraft, concerning fuel utilization and operating costs, were accomplished by considering: (1) incorporation of propfan performance and acoustic data; (2) revised mission profiles (longer design range and reduction in; and cruise speed) (3) utilization of alternate and advanced technology engines.
Document ID
19780013152
Acquisition Source
Legacy CDMS
Document Type
Contractor Report (CR)
Authors
Revell, J. D.
(Lockheed-California Co. Burbank, CA, United States)
Tullis, R. H.
(Lockheed-California Co. Burbank, CA, United States)
Date Acquired
September 3, 2013
Publication Date
August 1, 1977
Subject Category
Aircraft Design, Testing And Performance
Report/Patent Number
LR-28283
NASA-CR-152096
Report Number: LR-28283
Report Number: NASA-CR-152096
Accession Number
78N21095
Funding Number(s)
CONTRACT_GRANT: NAS2-8612
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.
No Preview Available