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Tank fragmentation testA photographic study of a simulated tank fragmentation test was made. Sixteen disks and four spheres were ejected from a test article mounted in a vertical orientation 110 ft above a target installed on the test chamber floor. The test was performed at a chamber pressure of 25 microns. Velocities at impingement on the target ranged from 88 to 120 ft/sec; corresponding ejection velocities at the exit plane of the ejector assembly ranged from 29 to 87 ft/sec. Tumble axes of the disks were expected to be all in the north-south direction; the majority of those measured were, while some were skewed from this direction, the maximum observed being 90 deg. A typical measured tumble rate was 2.4 turns/sec. The dispersion pattern measured on the target was reasonably regular, and measured approximately 16 ft east-to-west by 11 ft north-to-south.
Document ID
19730021210
Acquisition Source
Legacy CDMS
Document Type
Technical Memorandum (TM)
Authors
Daye, C. J.
(NASA Lewis Research Center Cleveland, OH, United States)
Cooksey, D.
(NASA Lewis Research Center Cleveland, OH, United States)
Walters, R. J.
(NASA Lewis Research Center Cleveland, OH, United States)
Auble, A. E.
(NASA Lewis Research Center Cleveland, OH, United States)
Date Acquired
September 2, 2013
Publication Date
August 1, 1973
Subject Category
Structural Mechanics
Report/Patent Number
NASA-TM-X-68282
Report Number: NASA-TM-X-68282
Accession Number
73N29942
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.
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