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Analytic Ballistic Performance Model of Whipple ShieldsThe dual-wall, Whipple shield is the shield of choice for lightweight, long-duration flight. The shield uses an initial sacrificial wall to initiate fragmentation and melt an impacting threat that expands over a void before hitting a subsequent shield wall of a critical component. The key parameters to this type of shield are the rear wall and its mass which stops the debris, as well as the minimum shock wave strength generated by the threat particle impact of the sacrificial wall and the amount of room that is available for expansion. Ensuring the shock wave strength is sufficiently high to achieve large scale fragmentation/melt of the threat particle enables the expansion of the threat and reduces the momentum flux of the debris on the rear wall. Three key factors in the shock wave strength achieved are the thickness of the sacrificial wall relative to the characteristic dimension of the impacting particle, the density and material cohesion contrast of the sacrificial wall relative to the threat particle and the impact speed. The mass of the rear wall and the sacrificial wall are desirable to minimize for launch costs making it important to have an understanding of the effects of density contrast and impact speed. An analytic model is developed here, to describe the influence of these three key factors. In addition this paper develops a description of a fourth key parameter related to fragmentation and its role in establishing the onset of projectile expansion.
Document ID
20150001652
Acquisition Source
Johnson Space Center
Document Type
Conference Paper
Authors
Miller, J. E.
(Texas Univ. El Paso, TX, United States)
Bjorkman, M. D.
(Jacobs Technology, Inc. Houston, TX, United States)
Christiansen, E. L.
(NASA Johnson Space Center Houston, TX, United States)
Ryan, S. J.
(Defence Science and Technology Organisation Fishermans Bend, Australia)
Date Acquired
February 13, 2015
Publication Date
April 26, 2015
Subject Category
Spacecraft Design, Testing And Performance
Report/Patent Number
JSC-CN-32626
Meeting Information
Meeting: Hypervelocity Impact Symposium
Location: Boulder, CO
Country: United States
Start Date: April 26, 2015
End Date: April 30, 2015
Sponsors: Hypervelocity Impact Society
Distribution Limits
Public
Copyright
Public Use Permitted.
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