Low Frequency Dynamical Behavior Of The Plasma At The Exit Plan Of A Hall Effect Thruster

A large research programme on Hall thrusters has been initiated in France in 1996. This programme includes modelling, as well as theoretical and experimental approaches. These researches are coordinated in the frame of a national Research Group. Recent results obtained at the laboratoire d'Aero...

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Bibliographische Detailangaben

Hauptverfasser:	Albarede, Luc, Vial, Vanessa, Lazurenko, Alexey, Bouchoule, Andre, Dudeck, Michel
Format:	Tagungsbericht
Sprache:	eng
Schlagworte:	70 PLASMA PHYSICS AND FUSION TECHNOLOGY ELECTRIC CURRENTS ELECTRIC POTENTIAL ELECTRONS ELECTROSTATIC PROBES HALL EFFECT IONS MAGNETOHYDRODYNAMICS PLASMA PROPULSION THRUSTERS TIME RESOLUTION
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