DOI: 10.26686/wgtn.26132662
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A Central-Cathode Electrostatic Thruster Featuring a High-Temperature Superconducting Applied Field Module

Christopher Acheson

Abstract: <p><strong>In recent decades, advances in electric propulsion have enabled the development of novel mission designs for space exploration. However, future deep space mission payloads of unprecedented mass will require advances in high thrust, high specific impulse propulsion. To achieve higher thrust density than traditional ion thrusters or Hall effect thrusters, novel designs for central-cathode electrostatic thrusters (CC-ESTs) and applied field magnetoplasmadynamic thrusters incorporate an appl… Show more

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