Magnesium Hall Thruster with Active Thermal Mass Flow Control

An active thermal mass flow control system for condensable propellant Hall-effect thrusters was demonstrated. The control system has the ability to arrest thermal runaway in a direct evaporation feed system and stabilize the discharge current during voltage-limited operation of a 2 kW magnesium-fuel...

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Veröffentlicht in:	Journal of propulsion and power 2014-05, Vol.30 (3), p.637-644
Hauptverfasser:	Hopkins, Mark A, King, Lyon B
Format:	Artikel
Sprache:	eng
Schlagworte:	Active control Algorithms Anode effect Anodes Automatic control Control algorithms Control systems Control theory Discharge Electric potential Feed systems Flow control Hall effect Heaters Heating equipment Magnesium Mass flow Plasma jets Proportional integral derivative Stability Steady state Thermal runaway Thrust Thrusters Voltage
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