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Development and simulation study of a new inverse-pinch high Coulomb transfer switchThe inverse-pinch plasma switch was studied using a computer simulation code. The code was based on a 2-D, 2-temperature magnetohydrodynamic (MHD) model. The application of this code was limited to the disk-type inverse-pinch plasma switch. The results of the computer analysis appear to be in agreement with the experimental results when the same parameters are used. An inverse-pinch plasma switch for closing has been designed and tested for high-power switching requirements. An azimuthally uniform initiation of breakdown is a key factor in achieving an inverse-pinch current path in the switch. Thus, various types of triggers, such as trigger pins, wire-brush, ring trigger, and hypocycloidal-pinch (HCP) devices have been tested for uniform breakdown. Recently, triggering was achieved by injection of a plasma-ring (plasma puff) that is produced separately with hypocycloidal-pinch electrodes placed under the cathode of the main gap. The current paths at switch closing, initiated by the injection of a plasma-ring from the HCP trigger are azimuthally uniform, and the local current density is significantly reduced, so that damage to the electrodes and the insulator surfaces is minimized. The test results indicate that electron bombardment on the electrodes and the insulator surfaces is minimized. The test results indicate that electron bombardment on the electrodes is four orders of magnitude less than that of a spark-gap switch for the same switching power. Indeed, a few thousand shots with peak current exceeding a mega-ampere and with hold-off voltage up to 20 kV have been conducted without showing measurable damage to the electrodes and insulators.
Document ID
19890013929
Acquisition Source
Legacy CDMS
Document Type
Contractor Report (CR)
Authors
Choi, Sang H.
(Information and Control Systems, Inc. Hampton, VA, United States)
Date Acquired
September 5, 2013
Publication Date
May 1, 1989
Subject Category
Plasma Physics
Report/Patent Number
NASA-CR-181768
NAS 1.26:181768
FR-688102
Report Number: NASA-CR-181768
Report Number: NAS 1.26:181768
Report Number: FR-688102
Accession Number
89N23300
Funding Number(s)
CONTRACT_GRANT: NAS1-17685
PROJECT: RTOP 506-41-41-02
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.
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