DocumentCode :
2785950
Title :
The performance analysis of power processing unit for electrojet plasma thrusters of space crafts
Author :
Mikhailov, M.V.
Author_Institution :
Sci. & Ind. Center, POLYPUS, Russia
fYear :
2000
fDate :
2000
Firstpage :
20
Lastpage :
21
Abstract :
At the present time, modern spacecraft have an onboard orbit raising thrusters system (ORTS). Many ORTSs contain electrojet plasma thrusters. The power processing unit is an obligatory part of any ORTS. It ensures the required electropower modes to all stationary plasma thruster elements. Here, the author presents a method for the performance analysis of spacecraft electrojet plasma thruster power processing units
Keywords :
aerospace propulsion; plasma jets; space vehicle power plants; electropower modes; orbit raising thrusters system; performance analysis; power processing unit; spacecraft electrojet plasma thrusters; stationary plasma thruster; Anodes; Cathodes; Electrodes; Filters; Ignition; Inverters; Performance analysis; Plasma applications; Plasma materials processing; Voltage;
fLanguage :
English
Publisher :
ieee
Conference_Titel :
Modern Techniques and Technology, 2000. MTT 2000. Proceedings of the VI International Scientific and Practical Conference of Students, Post-graduates and Young Scientists
Conference_Location :
Tomsk
Print_ISBN :
0-7803-5789-2
Type :
conf
DOI :
10.1109/SPCMTT.2000.896025
Filename :
896025
Link To Document :
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