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Space technology / Ion thruster / Hall effect thruster / Specific impulse / Propellant / Field-emission electric propulsion / Nanoparticle / Electrically powered spacecraft propulsion / Variable Specific Impulse Magnetoplasma Rocket / Spacecraft propulsion / Aerospace engineering / Propulsion


System Advantages of Nanoparticle Electric Propulsion
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Document Date: 2007-03-14 15:00:16


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City

Princeton / El Segundo / Reston / Cleveland / /

Company

Microcosm Press / Art Electric Propulsion Systems / Shimizu / Lehman / Electric Propulsion Laboratory / 5Space Systems / /

Country

Japan / /

Currency

USD / /

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Facility

NASA Lewis Research Center / NASA Institute / NASA Glenn Research Center / American Institute of Physics / University of Michigan / /

IndustryTerm

nano-electromechanical systems / low energy / space systems / dielectric liquid configuration using silicone oil / electrostatic thruster technology / propulsion systems / energy loss / power processing / sufficient energy / conventional chemical rockets / high energy / energy losses / in situ manufacturing sites / micro/nano-electromechanical systems / /

Organization

American Institute of Physics / University of Michigan / Ann Arbor / Technology Validation Mission / National Aeronautics and Space Administration / NASA Institute for Advanced Concepts / NASA Glenn Research Center / ON PP / the University of Michigan / /

Person

Matthew Forsyth / /

/

Product

Impulse / /

ProvinceOrState

New Jersey / Ohio / Virginia / California / Michigan / /

Technology

electrostatic thruster technology / EP technologies / MEMS / remote sensing / dielectric / ISP / ESA / MEMS technology / EP technology / /

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