Current leakage for low altitude satellites - Modeling applicationsTo simulate the behavior of a high voltage solar cell array in the ionospheric plasma environment, the large (90 ft x 55 ft diameter) vacuum chamber was used to measure the high-voltage plasma interactions of a 3 ft x 30 ft conductive panel. The chamber was filled with Nitrogen and Argon plasma at electron densities of up to 1,000,000 per cu cm. Measurements of current flow to the plasma were made in three configurations: (a) with one end of the panel grounded, (b) with the whole panel floating while a high bias was applied between the ends of the panel, and (c) with the whole panel at high negative voltage with respect to the chamber walls. The results indicate that a simple model with a constant panel conductivity and plasma resistance can adequately describe the voltage distribution along the panel and the plasma current flow. As expected, when a high potential difference is applied to the panel ends more than 95% of the panel floats negative with respect to the plasma.
Document ID
19800031796
Acquisition Source
Legacy CDMS
Document Type
Other - Collected Works
Authors
Konradi, A. (NASA Lyndon B. Johnson Space Center Houston, TX, United States)
Mccoy, J. E. (NASA Lyndon B. Johnson Space Center Houston, TX, United States)
Garriott, O. K. (NASA Johnson Space Center Houston, Tex., United States)