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Ablative shielding for hypervelocity projectilesA hypervelocity projectile shield which includes a hollow semi-flexible housing fabricated from a plastic like, or otherwise transparent membrane which is filled with a fluid (gas or liquid) is presented. The housing has a inlet valve, similar to that on a tire or basketball, to introduce an ablating fluid into the housing. The housing is attached by a Velcro mount or double-sided adhesive tape to the outside surface of a structure to be protected. The housings are arrayed in a side-by-side relationship for complete coverage of the surface to be protected. In use, when a hypervelocity projectile penetrates the outer wall of a housing it is broken up and then the projectile is ablated as it travels through the fluid, much like a meteorite 'burns up' as it enters the earth's atmosphere, and the housing is deflated. The deflated housing can be easily spotted for replacement, even from a distance. Replacement is then accomplished by simply pulling a deflated housing off the structure and installing a new housing.
Document ID
19930019899
Acquisition Source
Legacy CDMS
Document Type
Other - Patent
Authors
Rucker, Michelle A.
(NASA Lyndon B. Johnson Space Center Houston, TX, United States)
Date Acquired
August 15, 2013
Publication Date
June 8, 1993
Subject Category
Nonmetallic Materials
Report/Patent Number
Patent Number: US-PATENT-5,217,185
Patent Number: NASA-CASE-MSC-21884-1
Patent Application Number: US-PATENT-APPL-SN-887674
Accession Number
93N29088
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.
Patent
US-PATENT-5,217,185|NASA-CASE-MSC-21884-1
Patent Application
US-PATENT-APPL-SN-887674
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