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dc.contributor.authorDumont, Jean-Marie
dc.contributor.authorHansman, Robert J., Jr.
dc.contributor.authorReynolds, Thomas G.
dc.contributor.authorHansman, Robert J., Jr.
dc.contributor.authorHansman, Robert J., Jr.
dc.date.accessioned2015-05-13T14:04:09Z
dc.date.available2015-05-13T14:04:09Z
dc.date.issued2011-09
dc.identifier.isbn978-1-60086-941-9
dc.identifier.urihttp://hdl.handle.net/1721.1/96977
dc.description.abstractChanging aircraft operational procedures is one strategy that can be used to reduce fuel burn and mitigate environmental impacts of aviation in relatively short timeframes with existing aircraft types. This study quantifies the fuel burn and emissions reduction potential of delayed deceleration approaches, where the aircraft is kept fast and in clean aerodynamic configuration for as long as possible during the approach phase of flight. This reduces the drag and thrust requirements and these procedures are therefore called Low Power/Low Drag approaches. Operational data is used to characterize approach profiles, together with their fuel burn and emissions properties correlated to airspeed and configuration for a selection of aircraft types. Aircraft that were observed to decelerate and configure flaps later in the approach had 30-40% lower fuel burn and carbon dioxide emissions below 10,000 ft compared to those that did not. Estimates of US system-wide fuel burn and emissions reduction potential from Low Power/Low Drag approaches are provided: if only 1% of the total operations used these approaches, savings across all operators would amount to 2.9 million US gallons ($5.8-11.6 million at $2-4/US gallon) of fuel and 28,000 metric tons of carbon dioxide emissions per year. A discussion is provided on the implementation barriers which need to be addressed if benefits are to be realized.en_US
dc.description.sponsorshipUnited States. Federal Aviation Administration (Award 06-C-NE-MIT, Amendment 017)en_US
dc.language.isoen_US
dc.publisherAmerican Institute of Aeronautics and Astronauticsen_US
dc.relation.isversionofhttp://dx.doi.org/10.2514/6.2011-6886en_US
dc.rightsCreative Commons Attribution-Noncommercial-Share Alikeen_US
dc.rights.urihttp://creativecommons.org/licenses/by-nc-sa/4.0/en_US
dc.sourceHansmanen_US
dc.titleFuel Burn and Emissions Reduction Potential of Low Power/Low Drag Approachesen_US
dc.typeArticleen_US
dc.identifier.citationDumont, Jean-Marie, Tom Reynolds, and R John Hansman. “Fuel Burn and Emissions Reduction Potential of Low Power/Low Drag Approaches.” 11th AIAA Aviation Technology, Integration, and Operations (ATIO) Conference (September 20, 2011).en_US
dc.contributor.departmentLincoln Laboratoryen_US
dc.contributor.departmentMassachusetts Institute of Technology. Department of Aeronautics and Astronauticsen_US
dc.contributor.mitauthorDumont, Jean-Marieen_US
dc.contributor.mitauthorReynolds, Thomas G.en_US
dc.contributor.mitauthorHansman Jr., Robert J.en_US
dc.relation.journalProceedings of the 11th AIAA Aviation Technology, Integration, and Operations (ATIO) Conferenceen_US
dc.eprint.versionAuthor's final manuscripten_US
dc.type.urihttp://purl.org/eprint/type/ConferencePaperen_US
eprint.statushttp://purl.org/eprint/status/NonPeerRevieweden_US
dspace.orderedauthorsDumont, Jean-Marie; Reynolds, Tom; Hansman, R Johnen_US
dc.identifier.orcidhttps://orcid.org/0000-0002-9591-3579
dspace.mitauthor.errortrue
mit.licenseOPEN_ACCESS_POLICYen_US
mit.metadata.statusComplete


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