NASA NTRS · 19920000378
A Segmented Ion-Propulsion Engine
Abstract
New design approach for high-power (100-kW class or greater) ion engines conceptually divides single engine into combination of smaller discharge chambers integrated to operate as single large engine. Analogous to multicylinder automobile engine, benefits include reduction in required accelerator system span-to-gap ratio for large-area engines, reduction in required hollow-cathode emission current, mitigation of plasma-uniformity problem, increased tolerance to accelerator system faults, and reduction in vacuum-system pumping speed.
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Brophy, John R.. 1992-06-01. A Segmented Ion-Propulsion Engine. https://ntrs.nasa.gov/citations/19920000378
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