NASA NTRS · 19760044006
Sonic spark chambers for cosmic-ray experiments
Abstract
The sonic spark chamber provides an attractive high resolution hodoscope for low flux cosmic ray experiments. Spark position is determined by measurement of the time of flight of the sonic shock front from the spark position to a number of piezoelectric transducers placed at the periphery of the chamber. For each spark, four quantities must be determined: the spark coordinates, the sound velocity, and the spark 'size'. By over-determining the four parameters, high accuracy is possible. With eight sonic transducers, air-gap spark positions were measured with an error of less than 100 microns everywhere over a 1 sq m region.
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Ahlen, S. P., Cartwright, B. G., Price, P. B., Tarle, G.. 1975-01-01. Sonic spark chambers for cosmic-ray experiments. https://ntrs.nasa.gov/citations/19760044006
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