Mathematical model of pulsed plasma thruster with a preionization helicon discharge
Aircraft engines and power generators
Аuthors
*, **, ***, ****Bauman Moscow State Technical University, MSTU, 5, bldg. 1, 2-nd Baumanskaya str., Moscow, 105005, Russia
*e-mail: kuzenov@ipmnet.ru
**e-mail: svryzhkov@gmail.com
***e-mail: sstifler@ya.ru
****e-mail: shumaev@student.bmstu.ru
Keywords:
helicon discharge, the mathematical model, non-uniform electric and magnetic fields, pulsed coaxial plasma acceleratorReferences
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