Modified Electromechanical Modeling and Parameters Analysis of Magnetoplasmadynamic Thruster

To predict the thrust of magnetoplasmadynamic thrusters (MPDTs), a modified electromechanical model was proposed and a comparison with experimental results is presented in this paper. The motion of propellant in the thruster was divided into two portions: the axial motion which was accelerated by th...

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Principais autores:	Yu Zhang, Jianjun Wu, Yang Ou, Jian Li, Sheng Tan
Format:	Artigo
Jezik:	Inglês
Izdano:	MDPI AG 2019-06-01
Serija:	Energies
Teme:	magnetoplasmadynamic thrusters electromechanical model thrust performance discharge current anode radius mass flow rate applied magnetic field strength
Online dostop:	https://www.mdpi.com/1996-1073/12/12/2428
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