DocumentCode
1897333
Title
Design considerations for a low jitter trigatron
Author
McPhee, Andrew J. ; MacGregor, Scott J.
Author_Institution
British Aerosp. Defence, Dynamics Div., Bristol, UK
fYear
1994
fDate
34396
Firstpage
42401
Lastpage
42404
Abstract
Since it was first described in 1946, the trigatron spark gap has found wide use as a triggered high voltage switch. This presentation considers some of the pertinent aspects involved in the efficient design of a high voltage, low jitter trigatron. The approach taken was to check the test methodology by evaluating the performance of an existing triggered switch. The information gained led to the design of an enhanced performance trigatron. The test switch used in the present study is described by Thornton (1989) and was driven by a 10 stage Marx generator. It was designed to withstand 500 kV in air and 1 MV in transformer oil. The trigger signal was derived from a single stage RC circuit discharged through a spark gap and a coaxial delay line. A capacitive trigger was taken from the erecting Marx to initiate the trigger circuit. The trigger pulse was inverted by a 1:1 inverting TLT, resulting in the optimum trigatron configuration of a positive trigger pulse with a negative main pulse
Keywords
design engineering; gas-discharge tubes; pulse generators; pulsed power technology; spark gaps; switchgear; 1 MV; 500 kV; HV switchgear; Marx generator; air; coaxial delay line; design; jitter; negative main pulse; performance; positive trigger pulse; pulsed power; single stage RC circuit; test methodology; transformer oil; trigatron spark gap;
fLanguage
English
Publisher
iet
Conference_Titel
Pulsed Power '94, IEE Colloquium on
Conference_Location
London
Type
conf
Filename
297383
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