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The Flight Track Noise Impact ModelTo meet its objective of assisting the U.S. aviation industry with the technological challenges of the future, NASA must identify research areas that have the greatest potential for improving the operation of the air transportation system. To accomplish this, NASA is building an Aviation System Analysis Capability (ASAC). The Flight Track Noise Impact Model (FTNIM) has been developed as part of the ASAC. Its primary purpose is to enable users to examine the impact that quieter aircraft technologies and/or operations might have on air carrier operating efficiency at any one of 8 selected U.S. airports. The analyst selects an airport and case year for study, chooses a set of flight tracks for use in the case, and has the option of reducing the noise of the aircraft by 3, 6, or 10 decibels. Two sets of flight tracks are available for each airport: one that represents actual current conditions, including noise abatement tracks, which avoid flying over noise-sensitive areas; and a second set that offers more efficient routing. FTNIM computes the resultant noise impact and the time and distance saved for each operation on the more efficient, alternate tracks. Noise impact is characterized in three ways: the size of the noise contour footprint, the number of people living within the contours, and the number of homes located in the same contours. Distance and time savings are calculated by comparing the noise abatement flight path length to the more efficient alternate routing.
Document ID
19970018388
Acquisition Source
Langley Research Center
Document Type
Contractor Report (CR)
Authors
Burn, Melissa
(Wyle Labs., Inc. Arlington, VA United States)
Carey, Jeffrey
(Wyle Labs., Inc. Arlington, VA United States)
Czech, Joseph
(Wyle Labs., Inc. Arlington, VA United States)
Wingrove, Earl R., III
(Logistics Management Inst. McLean, VA United States)
Date Acquired
September 6, 2013
Publication Date
April 1, 1997
Subject Category
Aeronautics (General)
Report/Patent Number
NASA-CR-201683
NAS 1.26:201683
LMI-NS602T3
Report Number: NASA-CR-201683
Report Number: NAS 1.26:201683
Report Number: LMI-NS602T3
Accession Number
97N20367
Funding Number(s)
PROJECT: RTOP 538-08-11-01
CONTRACT_GRANT: NAS2-14361
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.
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