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Hypervelocity gunA velocity amplifier system which uses both electric and chemical energy for projectile propulsion is provided in a compact hypervelocity gun suitable for laboratory use. A relatively heavy layer of a tamping material such as concrete encloses a loop of an electrically conductive material. An explosive charge at least partially surrounding the loop is adapted to collapse the loop upon detonation of the charge. A source of electricity charges the loop through two leads, and an electric switch which is activated by the charge explosive charge, disconnects the leads from the source of electricity and short circuits them. An opening in the tamping material extends to the loop and forms a barrel. The loop, necked down in the opening, forms the sabot on which the projectile is located. When the loop is electrically charged and the explosive detonated, the loop is short circuited and collapsed thus building up a magnetic field which acts as a sabot catcher. The sabot is detached from the loop and the sabot and projectile are accelerated to hypervelocity.
Document ID
19790012913
Acquisition Source
Legacy CDMS
Document Type
Other - Patent
Authors
Ford, F. C.
(MB Assoc. San Ramon, Calif., United States)
Biehl, A. J.
(NASA Lewis Research Center Cleveland, OH, United States)
Date Acquired
September 3, 2013
Publication Date
December 21, 1965
Subject Category
Research And Support Facilities (Air)
Report/Patent Number
Patent Number: US-PATENT-3,224,337
Patent Application Number: US-PATENT-APPL-SN-200770
Patent Number: NASA-CASE-XLE-03186-1
Accession Number
79N21084
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.
Patent
US-PATENT-3,224,337|NASA-CASE-XLE-03186-1
Patent Application
US-PATENT-APPL-SN-200770
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