NASA NTRS · 19660045229
Propellant injection into a coaxial plasma accelerator.
Abstract
Two propellant injector designs for plasma accelerators that minimize or avoid bearing seal difficulty, using piezoelectric element and pulsed vaporization of filament of liquid conductor
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Gloersen, P., Gorowitz, B., Karras, T. W.. 1966-03-01. Propellant injection into a coaxial plasma accelerator.. https://ntrs.nasa.gov/citations/19660045229
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