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Ballistic Limit Equation for Single Wall TitaniumHypervelocity impact tests and hydrocode simulations were used to determine the ballistic limit equation (BLE) for perforation of a titanium wall, as a function of wall thickness. Two titanium alloys were considered, and separate BLEs were derived for each. Tested wall thicknesses ranged from 0.5mm to 2.0mm. The single-wall damage equation of Cour-Palais [ref. 1] was used to analyze the Ti wall's shielding effectiveness. It was concluded that the Cour-Palais single-wall equation produced a non-conservative prediction of the ballistic limit for the Ti shield. The inaccurate prediction was not a particularly surprising result; the Cour-Palais single-wall BLE contains shield material properties as parameters, but it was formulated only from tests of different aluminum alloys. Single-wall Ti shield tests were run (thicknesses of 2.0 mm, 1.5 mm, 1.0 mm, and 0.5 mm) on Ti 15-3-3-3 material custom cut from rod stock. Hypervelocity impact (HVI) tests were used to establish the failure threshold empirically, using the additional constraint that the damage scales with impact energy, as was indicated by hydrocode simulations. The criterion for shield failure was defined as no detached spall from the shield back surface during HVI. Based on the test results, which confirmed an approximately energy-dependent shield effectiveness, the Cour-Palais equation was modified.
Document ID
20090007776
Acquisition Source
Johnson Space Center
Document Type
Extended Abstract
Authors
Ratliff, J. M.
(NASA Johnson Space Center Houston, TX, United States)
Christiansen, Eric L.
(NASA Johnson Space Center Houston, TX, United States)
Bryant, C.
(NASA Johnson Space Center Houston, TX, United States)
Date Acquired
August 24, 2013
Publication Date
January 1, 2009
Subject Category
Spacecraft Design, Testing And Performance
Report/Patent Number
JSC-17569
Report Number: JSC-17569
Meeting Information
Meeting: 5th European Conference on Space Debris
Location: Darmstadt
Country: Germany
Start Date: March 30, 2009
End Date: April 2, 2009
Sponsors: European Space Agency
Funding Number(s)
WBS: WBS 510505.05.05.05.03
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.
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