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Aerospace engineering / Propulsion / Electrodeless plasma thruster / Plasma propulsion engine / Electron cyclotron resonance / Plasma / Ponderomotive force / Ion source / Ion thruster / Spacecraft propulsion / Physics / Plasma physics


Development of a High Power Electrodeless Thruster
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Document Date: 2006-06-08 09:49:31

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File Size: 863,64 KB

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City

Philadelphia / Wilmington / New York / Paris / /

Company

The Elwing Company / Academia Press / EPPDy Laboratory / Concept & Structure The Elwing Company / Acknowledgments The Elwing Company / /

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Facility

Princeton University / /

IndustryTerm

energy density gradient2 / higher energy density / energy density gradient / overall devices / crossed energy density gradient / electromagnetic energy density1 / power devices / fundamental solutions / electric propulsion devices / allowed computing performance projections / microwave power coupling devices / lower electromagnetic energy density / high energy density area / electromagnetic energy density gradient / high energy density / energy density / electrodeless plasma thruster technology / electronics / high energy density area magnetic field / linear device / electromagnetic energy density / compact devices / electric propulsion systems / thermal management / lower energy density / energy / gas injection / /

Organization

US Federal Reserve / Princeton University / /

Person

Edgar Choueiri / G. Emsellem / S. Larigaldie / E. Rosencher / Gregory D. Emsellem / /

Position

author / Chief Scientist / General / /

ProvinceOrState

Delaware / New York / /

Technology

radiation / electrodeless plasma thruster technology / dielectric / microwave / ISP / simulation / /

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