Back to Results
First PageMeta Content
Plasma / Technology / Ion thruster / Electrostatic ion thruster / Spacecraft propulsion / Physics / Hall effect thruster


APPLIED PHYSICS LETTERS 90, 221502 共2007兲 Enhanced performance of cylindrical Hall thrusters Y. Raitses,a兲 A. Smirnov, and N. J. Fisch Princeton Plasma Physics Laboratory, Princeton University, Princeton, New Jers
Add to Reading List

Document Date: 2007-12-03 15:56:39


Open Document

File Size: 375,87 KB

Share Result on Facebook

City

Pyung Chang / Reston / Jerusalem / Sacramento / /

Country

Korea / Israel / /

Currency

USD / /

/

Facility

Princeton University / American Institute of Physics Downloaded / Hall thruster / 1 i.e. / Hall thrusters1 / 2 / American Institute of Physics / American Institute of Aeronautics / N. J. Fisch Princeton Plasma Physics Laboratory / Two laboratory CHTs / /

IndustryTerm

peak ion energy / gas flow rate / high-energy ions / plume diagnostic tools / given gas flow rate / energy ions / low power space applications / xenon gas flow rate / anode gas flow rate / energy / ion energy distribution function / /

Organization

Congress / American Institute of Physics / American Institute of Aeronautics and Astronautics / 82nd Korean Physical Society / A. Smirnov / and N. J. Fisch Princeton Plasma Physics Laboratory / Princeton University / Air Force office of Scientific Research / /

Person

Edgar Choueiri / Leonid Dorf / Erik Granstedt / /

Position

Professor / RPA collector / /

ProvinceOrState

New Jersey / Virginia / /

PublishedMedium

APPLIED PHYSICS LETTERS / /

URL

http /

SocialTag