Examination of Annular-Electrode Spark Discharges in Flowing Oxygen - An Overview

Tinker, Darren C ; Osborne, Robin J ; Pitz, Robert W

关键词: GAS DISCHARGES;    ELECTRODES;    LIQUID PROPELLANT ROCKET ENGINES;   

RP-ID  :  M18-6791

学科分类：航空航天科学

美国|英语

来源: NASA Technical Reports Server

【 摘 要 】

A 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.