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Effect of Target Thickness on Cratering and Penetration of Projectiles Impacting at Velocities to 13,000 Feet Per SecondIn order to determine the effects of target thickness on the penetration and cratering of a target resulting from impacts by high-velocity projectiles, a series of experimental tests have been run. The projectile-target material combinations investigated were aluminum projectiles impacting aluminum targets and steel projectiles impacting aluminum and copper targets. The velocity spectrum ranged from 4,000 ft/sec to 13,000 ft/sec. It has been found that the penetration is a function of target thickness provided that the penetration is greater than 20 percent of the target thickness. Targets of a thickness such that the penetration amounts to less than 20 percent of the thickness may be regarded as quasi-infinite. An empirical formula has been established relating the penetration to the target thickness and to the penetration of a projectile of the same mass, configuration, and velocity into a quasi- infinite target. In particular, it has been found that a projectile can completely penetrate a target whose thickness is approximately one and one-half times as great as the penetration of a similar projectile into a quasi-infinite target. The diameter of a crater has also been found to be a function of the target thickness provided that the target thickness is not greater than the projectile length in the case of cylindrical projectiles and not greater than two to three times the projectile diameter in the case of spherical projectiles.
Document ID
19980231991
Acquisition Source
Headquarters
Document Type
Other - NASA Memorandum (MEMO)
Authors
Kinard, William H.
(NASA Langley Research Center Hampton, VA United States)
Lambert, C. H., Jr.
(NASA Langley Research Center Hampton, VA United States)
Schryer, David R.
(NASA Langley Research Center Hampton, VA United States)
Casey, Francis W., Jr.
(NASA Langley Research Center Hampton, VA United States)
Date Acquired
September 6, 2013
Publication Date
December 1, 1958
Subject Category
Structural Mechanics
Report/Patent Number
NASA-MEMO-10-18-58L
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.
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