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Aluminum runway surface as possible aid to aircraft brakingSeveral concepts are described for use singly or in combination to improve aircraft braking. All involve a thin layer of aluminum covering all or part of the runway. Advantage would derive from faster heat conduction from the tire-runway interface. Heating of tread surface with consequent softening and loss of friction coefficient should be reduced. Equations are developed indicating that at least 99 percent of friction heat should flow into the aluminum. Preliminary test results indicate a coefficient of sliding friction of 1.4, with predictably slight heating of tread. Elimination of conventional brakes is at least a remote possibility.
Document ID
19730009313
Acquisition Source
Legacy CDMS
Document Type
Other - NASA Technical Note (TN)
Authors
Miller, C. D.
(NASA Lewis Research Center Cleveland, OH, United States)
Pinkel, I. I.
(NASA Lewis Research Center Cleveland, OH, United States)
Date Acquired
September 2, 2013
Publication Date
March 1, 1973
Subject Category
Aircraft
Report/Patent Number
E-7046
NASA-TN-D-7186
Report Number: E-7046
Report Number: NASA-TN-D-7186
Accession Number
73N18040
Funding Number(s)
PROJECT: RTOP 501-38
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.
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