Back to Results
First PageMeta Content
Plasma / Hall effect thruster / Electric current / Electrodeless plasma thruster / Spacecraft propulsion / Plasma physics / Physics


JOURNAL OF APPLIED PHYSICS 99, 036103 共2006兲 Operation of a segmented Hall thruster with low-sputtering carbon-velvet electrodes Y. Raitses,a兲 D. Staack, A. Dunaevsky, and N. J. Fisch Princeton Plasma Physics Labo
Add to Reading List

Document Date: 2006-05-31 14:35:09

Open Document

File Size: 191,74 KB

Share Result on Facebook

City

Princeton / Reston / Cleveland / Indianapolis / London / San Diego / /

Company

HP / Energy Science Laboratories Inc. / /

Currency

USD / /

/

Facility

Hall thruster / 1 / 2 / American Institute of Physics Downloaded / American Institute of Physics / American Institute of Aeronautics / University of Michigan / N. J. Fisch Princeton Plasma Physics Laboratory / /

IndustryTerm

neutral gas flow / energy / /

Organization

Electric Rocket Propulsion Society / D. Staack / A. Dunaevsky / and N. J. Fisch Princeton Plasma Physics Laboratory / American Institute of Physics / American Institute of Aeronautics and Astronautics / University of Michigan / US DOE / /

Person

Leonid Dorf / Artem Smirnov / R. R. Hofer / J. D. Williams / John D. Williams / Timothy R. Knowles / /

Position

Professor / /

ProvinceOrState

New Jersey / Ohio / Virginia / Michigan / /

PublishedMedium

JOURNAL OF APPLIED PHYSICS / /

Technology

microwave / /

URL

http /

SocialTag