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Examination of Annular-Electrode Spark Discharges in Flowing Oxygen – Experimental NuancesMicrosecond sparks and the resulting plume of hot gas/plasma were examined against a parametric pressure-distance matrix. Schlieren imaging is used to capture the spatial and temporal location of spark discharge exhaust for two milliseconds. Low pressure and larger gap widths created the largest size and intensity signal for the spark-affected plumes. Experimental exit-plume velocities trend well with analytic predictions using a mean pressure between the chamber and atmospheric conditions. Due to the quadratic relation of the annulus area and gap width, larger gap width velocities are more accurately represented by analytic predictions using atmospheric pressure as the larger exit area restricts the flow less. The same pressure adjustment, when applied to breakdown voltages, improves data alignment with Paschen’s Curve.
Document ID
20190000726
Acquisition Source
Marshall Space Flight Center
Document Type
Conference Paper
Authors
Darren C Tinker
(Vanderbilt University Nashville, Tennessee, United States)
Marsalis Pullen
(Vanderbilt University Nashville, Tennessee, United States)
Robin J Osborne
(Jacobs (United States) Dallas, Texas, United States)
Robert W. Pitz
(Vanderbilt University Nashville, Tennessee, United States)
Date Acquired
February 14, 2019
Publication Date
January 11, 2019
Subject Category
Spacecraft Design, Testing And Performance
Report/Patent Number
M18-7126
Meeting Information
Meeting: AIAA Science and Technology Forum (AIAA SciTech 2019)
Location: San Diego, CA
Country: US
Start Date: January 7, 2019
End Date: January 11, 2019
Sponsors: American Institute of Aeronautics and Astronautics
Funding Number(s)
CONTRACT_GRANT: NNX16AM57H
Distribution Limits
Public
Copyright
Public Use Permitted.
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