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Physics / Ion thruster / Hall effect thruster / Inertial electrostatic confinement / Plasma / Ion source / Electrostatic ion thruster / Electrically powered spacecraft propulsion / Spacecraft propulsion / Aerospace engineering / Propulsion


Space Thruster Based on Inertial Electrostatic Confinement Benjamin A. Ulmen, Guilherme Amadio, Hugo Leon, George Chen, William W. Matisiak, Paul Keutelian, George H. Miley Introduction Theory of Operation
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Document Date: 2010-01-20 18:11:48


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File Size: 1,38 MB

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Company

Dell / /

Facility

University of Illinois / /

IndustryTerm

appropriate gas choice / correct energy / eventual energy generation / few practical applications / Energy selection / energy spectrum / low energy-per-ion cost / selected energy / light-weight metal grids / diagnostic tool / stage device / energy / /

Organization

University of Illinois / /

Person

Paul Keutelian / Hugo Leon / George Chen / William W. Matisiak / M. P. Reilly / V / William A. Hargus / Benjamin A. Ulmen / George H. Miley / /

ProvinceOrState

Illinois / /

Technology

ISP / ESA / /

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