Design of a Low-Energy FARAD Thruster

The design of an electrodeless thruster that relies on a pulsed, rf-assisted discharge and electromagnetic acceleration using an inductive coil is presented. The thruster design is optimized using known performance,scaling parameters, and experimentally-determined design rules, with design targets f...

Ausführliche Beschreibung

Bibliographische Detailangaben

Hauptverfasser:	Polzin, K. A., Rose, M. F., Miller, R., Best, S., Owens, T., Dankanich, J.
Format:	Tagungsbericht
Sprache:	eng
Schlagworte:	Spacecraft Propulsion And Power
Online-Zugang:	Volltext bestellen
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