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Follow-On Technology Requirement Study for Advanced Subsonic TransportA study was conducted to define and assess the critical or enabling technologies required for a year 2005 entry into service (EIS) engine for subsonic commercial aircraft, with NASA Advanced Subsonic Transport goals used as benchmarks. The year 2005 EIS advanced technology engine is an Advanced Ducted Propulsor (ADP) engine. Performance analysis showed that the ADP design offered many advantages compared to a baseline turbofan engine. An airplane/ engine simulation study using a long range quad aircraft quantified the effects of the ADP engine on the economics of typical airline operation. Results of the economic analysis show the ADP propulsion system provides a 6% reduction in direct operating cost plus interest, with half the reduction resulting from reduced fuel consumption. Critical and enabling technologies for the year 2005 EIS ADP were identified and prioritized.
Document ID
20030067946
Acquisition Source
Glenn Research Center
Document Type
Contractor Report (CR)
Authors
Wendus, Bruce E.
(United Technologies Corp. West Palm Beach, FL, United States)
Stark, Donald F.
(United Technologies Corp. West Palm Beach, FL, United States)
Holler, Richard P.
(United Technologies Corp. West Palm Beach, FL, United States)
Funkhouser, Merle E.
(United Technologies Corp. West Palm Beach, FL, United States)
Date Acquired
September 7, 2013
Publication Date
August 1, 2003
Subject Category
Aircraft Propulsion And Power
Report/Patent Number
NAS 1.26:212467
NASA/CR-2003-212467
E-14005
Report Number: NAS 1.26:212467
Report Number: NASA/CR-2003-212467
Report Number: E-14005
Funding Number(s)
CONTRACT_GRANT: NAS3-26618
WORK_UNIT: WU-538-06-11-00
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.
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