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Multiple-Purpose Subsonic Naval Aircraft (MPSNA) Multiple Application Propfan Study (MAPS)A conceptual design study compared a selected propfan-powered aircraft to a turbofan-powered aircraft for multiple Navy carrier-based support missions in the 1995 timeframe. Conventional takeoff and landing (CTOL) propfan and turbofan-powered designs and short takeoff/vertical landing (STOVL) propfan-powered designs are presented. Ten support mission profiles were defined and the aircraft were sized to be able to perform all ten missions. Emphasis was placed on efficient high altitude loiter for Airborne Early Warning (AEW) and low altitude high speed capability for various offensive and tactical support missions. The results of the study show that the propfan-powered designs have lighter gross weights, lower fuel fractions, and equal or greater performance capability than the turbofan-powered designs. Various sensitives were developed in the study, including the effect of using single-rotation versus counter-rotation propfans and the effect of AEW loiter altitude on vehicle gross weight and empty weight. A propfan technology development plan was presented which illustrates that the development of key components can be achieved without accelerated schedules through the extension of current and planned government and civil propfan programs.
Document ID
19890009918
Acquisition Source
Legacy CDMS
Document Type
Contractor Report (CR)
Authors
Winkeljohn, D. M.
(Lockheed-Georgia Co. Marietta, GA, United States)
Mayrand, C. H.
(Lockheed-Georgia Co. Marietta, GA, United States)
Date Acquired
September 5, 2013
Publication Date
March 1, 1986
Subject Category
Aircraft Design, Testing And Performance
Report/Patent Number
NAS 1.26:175096
LG86ER0053
NASA-CR-175096
Accession Number
89N19289
Funding Number(s)
PROJECT: RTOP 535-03-01
CONTRACT_GRANT: NAS3-24528
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.
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