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Lightweight tire concept for space shuttleVarious tests were conducted on a 49x17/26 PR aircraft tire that had been designed as a lightweight tire for use on the C-5A military transport. This tire is approximately 25 per cent lighter than a tire of the same size and ply rating that would be used in commercial airline service. The tires were tested at 40 per cent, 37 per cent, and 35 per cent deflections. These deflections were obtained by adjusting the inflation pressure while the load on the tire remained constant at 60,000 pounds. It was determined that the tire would operate successfully under the test conditions at 35% deflection. Prior to testing, the tires were subjected to conditions of high vacuum and low temperature. It was determined that the tires were not adversely affected by these conditions.
Document ID
19740004388
Acquisition Source
Legacy CDMS
Document Type
Contractor Report (CR)
Authors
Shufflebotham, W. T.
(Goodrich (B. F.) Co. Akron, OH, United States)
Date Acquired
September 3, 2013
Publication Date
October 30, 1973
Subject Category
Space Vehicles
Report/Patent Number
NASA-CR-134127
ATD-2751
Report Number: NASA-CR-134127
Report Number: ATD-2751
Accession Number
74N12501
Funding Number(s)
CONTRACT_GRANT: NAS9-12049
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.
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