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Multiple Application Propfan Study (MAPS): Advanced tactical transportThis study was conducted to ascertain potential benefits of a propfan propulsion system application to a blended wing/body military tactical transport. Based on a design cruise Mach no. of 0.75 for the design mission, the results indicate a significant advantage in various figures of merit for the propfan over those of a comparable technology turbofan. Although the propfan has a 1.6 percent greater takeoff gross weight, its life cycle cost is 5.3 percent smaller, partly because of a 27 percent smaller specific fuel consumption. When employed on alternate missions, the propfan configuration offers significantly improved flexibility and capability: an increase in sea level penetration distance of more than 100 percent, or in time-on-station of 24 percent, or in deployment payload of 38 percent.
Document ID
19890009929
Acquisition Source
Legacy CDMS
Document Type
Contractor Report (CR)
Authors
Newton, F. C.
(Douglas Aircraft Co., Inc. Long Beach, CA, United States)
Liebeck, R. H.
(Douglas Aircraft Co., Inc. Long Beach, CA, United States)
Mitchell, G. H.
(Douglas Aircraft Co., Inc. Long Beach, CA, United States)
Mooiweer, A.
(Douglas Aircraft Co., Inc. Long Beach, CA, United States)
Platte, M. M.
(Douglas Aircraft Co., Inc. Long Beach, CA, United States)
Toogood, T. L.
(Douglas Aircraft Co., Inc. Long Beach, CA, United States)
Wright, R. A.
(Douglas Aircraft Co., Inc. Long Beach, CA, United States)
Date Acquired
September 5, 2013
Publication Date
March 1, 1986
Subject Category
Aircraft Propulsion And Power
Report/Patent Number
NASA-CR-175003
NAS 1.26:175003
Report Number: NASA-CR-175003
Report Number: NAS 1.26:175003
Accession Number
89N19300
Funding Number(s)
CONTRACT_GRANT: NAS3-24348
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.
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