1 kW Laboratory Hall Thruster
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Thruster channel Material:
Boron nitride
Input
power range: 0.4-1 kW Discharge
voltage: 200-400 V Flow rate
(Xenon): 15-30 sccm Thrust:
20-50 mN Isp:
1200-2000 sec
Efficiency: 30 – 55%
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This is the first PPPL Hall thruster designed and built in 1999. It has an original flexible design with two electromagnets (inner and outer) and shaped magnetic screen to allow an extended operating range (>1 kW). Our initial results on the effects of segmented electrodes were obtained for this thruster. |
Copyright © 2003 Princeton Plasma Physics Laboratory