کد مقاله | کد نشریه | سال انتشار | مقاله انگلیسی | نسخه تمام متن |
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5028746 | 1470641 | 2017 | 5 صفحه PDF | دانلود رایگان |
EDB Fakel has designed and operates a plasma cathode-compensator operating at Xenon flow rate of 0.15-0.20 mg/s at the discharge current of 1.25 A as a part of a 225 W powered SPT-50 stationary plasma thruster. After starting the thruster, the cathode requires no additional warm-up and its thermal mode is sustained by the discharge current. Such thrusters and cathodes are used on “Kanopus” spacecraft.When switching to high-voltage modes with a decreased discharge current the use of LaB6 as an emissive material poses difficulties, as the thermal power emitted on the thermoemitter is not sufficient for operation in a self-sustained mode. Emissive materials based on BaO, which are widely used abroad, are more suitable for discharge currents in the range of 0.4-1.0 A. Such material has been developed and tested as a part of a laboratory model.The results of the experimental test are presented below.
Journal: Procedia Engineering - Volume 185, 2017, Pages 80-84