MAGNETOPLASMADYNAMIC THRUSTOR RESEARCH

This program is a follow-on study to a three-year feasibility investigation of using lithium propellant in a steady state electric plasma thrustor for eventual use in space propulsion. During that program, accelerator development was largely empirical. The present research is aimed at obtaining a de...

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Bibliographische Detailangaben
Hauptverfasser:	Cann, G L, Nelson, S T, Harder, R L, Jacobs, P F
Format:	Report
Sprache:	eng
Schlagworte:	ALKALI PLASMA HALL ACCELERATORS ANODES CATHODES Electric and Ion Propulsion ELECTRIC PROPULSION ELECTRODES FEASIBILITY STUDIES IONIZATION LITHIUM MAGNETIC FIELDS MAGNETOHYDRODYNAMICS OSCILLATION PLASMA ACCELERATORS PLASMA ENGINES Plasma Physics and Magnetohydrodynamics PLASMAS(PHYSICS) PROPELLANTS SPECIFIC IMPULSE THRUST
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