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NASA NTRS ยท 19750029453

A spark gap switching system for gasdynamic facilities

Abstract

A spark gap switching system has been developed to coordinate the discharge of a 300 kJ capacitor bank with the high speed flow of helium in a shock tube driver. The trigger system includes a flow transducer, a pulse forming circuit, a high voltage spark generator, and four heavy duty spark gaps that can carry total peak currents greater than 1.5 million A. A glow gauge flow transducer sensitive to small gas density changes was used whose input power and signal output can withstand high voltage fluctuations. This switching system is of use with gasdynamic discharge devices requiring a minimum number of switches.

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BibTeXRIS

Leibowitz, L. P.. 1974-11-01. A spark gap switching system for gasdynamic facilities. https://ntrs.nasa.gov/citations/19750029453

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