Experimental and Numerical Examination of the BHT-200 Hall Thruster Plume (Preprint)

The plume of a Busek BHT-200 xenon Hall thruster has been characterized through measurements from various plasma electrostatic probes. Ion current flux, plasma potential, plasma density, and electron temperatures were measured in the near-field of the plume to 60 cm downstream of the exit plane. The...

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Bibliographische Detailangaben
Hauptverfasser:	Nakles, Michael R, Brieda, Lubos, Reed, Garrett, Hargus, William A, Spicer, Randy L
Format:	Report
Sprache:	eng
Schlagworte:	Computer Programming and Software COMPUTERIZED SIMULATION DRACO PLASMA PLUME CODE Electric and Ion Propulsion EXPERIMENTAL DESIGN HALL THRUSTERS MATHEMATICAL MODELS PLASMA ELECTROSTATIC PROBES Plasma Physics and Magnetohydrodynamics PLASMAS(PHYSICS) PLUME PROPERTIES PLUMES SYMPOSIA Test Facilities, Equipment and Methods WUAFRL33SP0706 XENON
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