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Examination of Annular-Electrode Spark Discharges in Flowing Oxygen - An OverviewA parametric study of annular spark gaps, pressures, and spark discharges in flowing oxygen gas was performed with a Champion spark exciter. The range of the pressure-distance product for the experiment is from approximately 50 torr-cm to 2500 torr-cm. Measurements of breakdown voltage qualitatively trend with Paschen's curve. Spark duration remained constant until the pressure-distance product exceeded 200 torr-cm, and then steadily increased. The mean spark energy increases linearly with the pressure-distance on a log-log plot indicating that a definite power relationship exists. The distribution of sparks at low energies and low pressures is not Gaussian and has no dominant peaks. Moderate and high spark energies are bimodal, with the dominant mode near 80 mJ. As pressure increases, dominant and secondary modes approach the same probability.
Document ID
20180006340
Acquisition Source
Marshall Space Flight Center
Document Type
Conference Paper
Authors
Darren C. Tinker
(Vanderbilt University Nashville, Tennessee, United States)
Robin J .Osborne
(ERC, Inc. Dallas, Texas, United States)
Robert W. Pitz
(Vanderbilt University Nashville, Tennessee, United States)
Date Acquired
October 17, 2018
Publication Date
July 10, 2018
Subject Category
Spacecraft Propulsion And Power
Report/Patent Number
M18-6791
Meeting Information
Meeting: 2018 AIAA Propulsion and Energy Forum and Exposition
Location: Cincinnati, OH,
Country: United States
Start Date: July 9, 2018
End Date: July 11, 2018
Sponsors: American Inst. of Aeronautics and Astronautics
Funding Number(s)
CONTRACT_GRANT: NNX16AM57H
Distribution Limits
Public
Copyright
Public Use Permitted.
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