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Electromagnetism / Ions / Ion thruster / Hall effect thruster / Aerospace engineering / Plasma / Ion source / Langmuir probe / Double layer / Spacecraft propulsion / Physics / Plasma physics


Document Date: 2003-05-19 12:12:37

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City

Orlando / Amsterdam / Kitakyushu / New York / /

Company

Millipore / HALL THRUSTER DIAGNOSTICS / /

Country

Japan / Netherlands / /

Currency

USD / /

Facility

Princeton University / American Institute of Physics Downloaded / American Institute of Physics / N. J. Fisch Princeton Plasma Physics Laboratory / /

IndustryTerm

propellant gas / Gas flow rates / gas velocity / gas flow rate / research grade xenon gas / gas inlet / thermal energy / travel way / kinetic energy eV acl / gas distributor / xenon gas flow rate / energy / /

Organization

American Institute of Physics / N. J. Fisch Princeton Plasma Physics Laboratory / Consultants Bureau / Princeton University / U.S. Securities and Exchange Commission / /

Person

I. Kaganovich / M. A. Capelli / D. R. Shmidt / N. B. Meezan / W. A. Hargus / Jr. / /

Position

conductor / Invited speaker / representative / /

ProvinceOrState

New Jersey / Florida / New York / /

Technology

dielectric / /

URL

http /

SocialTag