A vacuum arc thruster (VAT) is a form of electric spacecraft propulsion. It uses a vacuum arc discharge, across an insulator, between two electrodes to produce thrust.[1] A metal plasma is produced from micrometer-size cathodic spots. Thus, whereas the insulator is used as propellant in a pulsed plasma thruster, in a VAT the metallic cathode is consumed as propellant.
^Lunn, Jonathan (17 November 2016). "Vacuum Arc Thruster and Method of Operating the Same". WIPO IP Portal. Retrieved 20 October 2020.
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A vacuumarcthruster (VAT) is a form of electric spacecraft propulsion. It uses a vacuumarc discharge, across an insulator, between two electrodes to...
between the electrodes. Cathodic arc deposition Electric arc Electric discharge in gases Glow discharge Vacuumarcthruster Messyats, Gennady A.; Proskurovsky...
other forms of electric propulsion such as Hall-effect ion thrusters. Vacuumarcthruster "NASA Glenn Research Center PPT". National Aeronautics & Space...
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Anflo, K.; Moore, S.; King, P. Expanding the ADN-based Monopropellant Thruster Family. 23rd Annual AIAA/USU Conference on Small Satellites. SSC09-II-4...
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