NASA NTRS · 19890029110
Cathode phenomena in a low power, steady state MPD thruster
Abstract
Mass loss and surface temperature measurements, filter photography and SEM surface characterization are used to study cathode phenomena in a steady state self-field MPD thruster operated at power levels between 15 and 30 kW. The equilibrium cathode temperature is found to be approximately 3200 K over most of its length, for which evaporation and thermionic emission adequately explain measured erosion rates and current levels. The start-up phase is characterized by spot current attachment with associated high erosion rates.
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Kelly, A. J., Jahn, R. G., Myers, R. M., Suzuki, N.. 1988-07-01. Cathode phenomena in a low power, steady state MPD thruster. https://ntrs.nasa.gov/citations/19890029110
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