Results 11 to 20 of about 9,251 (208)
Review of Plasma-Induced Hall Thruster Erosion
The Hall thruster is a high-efficiency spacecraft propulsion device that utilizes plasma to generate thrust. The most common variant of the Hall thruster is the stationary plasma thruster (SPT).
Nathan P. Brown, Mitchell L. R. Walker
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Effects of Magnetic Shielding Configuration on Discharge Characteristics and Performance of a 60 mm-Diameter Low-Power Hall Thruster [PDF]
Lifetime is a main factor restraining the application of low-power Hall thruster. Magnetic shielding configuration is regarded as a promising method to prolong the lifespan of Hall thruster.
Weilong Guo +4 more
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Influences of Magnetic Flux Density on Discharge Characteristics of Low-Power Hall Thruster [PDF]
The design of the magnetic field is crucial to the performance of the hall thruster. This paper investigates the effects of magnetic field on the discharge characteristics of the low-power hall thruster in the method of combining simulation and ...
Weilong Guo, Jun Gao, Zuo Gu, Ning Guo
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Study on the influence of magnetic field on the performance of a 5 kW hall thruster
Hall thruster is a kind of plasma optics device, which is used mainly in space propulsion. To study the influence of magnetic field on the performance of a 5 kW hall thruster, a two-dimensional PIC-MCC model was built.
L. Yang, P. Y. Wang, T. Wang
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Simulation of Hollow Cathode in the Hall Thruster by Particle in Cell (PIC) Method [PDF]
The this article the characteristics of the hollow cathode plasma particles in the spt-100 hall effect thruster have been investigated by two-dimensional particle-in-cell simulation. One of the main and important components of the hall thruster is hollow
masumeh kiantaj +3 more
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An integrated fluid simulation platform on Hall thruster plasmas
In this work, a newly integrated fluid simulation platform, named DUT-HTFS, is developed for the multiple physical fields in Hall thrusters. The integrated simulation platform includes three inter-related parts: the geometry module, background magnetic ...
Nannan Li +3 more
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The lifetime of electric propulsion (EP) thrusters depends particularly on the erosion characteristics of operation relevant components, for instance, the grid hole erosion of gridded ion thrusters or the channel wall erosion of Hall effect thrusters ...
Carsten Bundesmann +8 more
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PIC-DSMC Simulation of a Hall Thruster Plume with Charge Exchange Effects Using pdFOAM
To develop technologies for the stable operation of electric propulsion systems, the effects of charge exchange (CEX) on the exhaust plume of a Hall thruster were studied using the particle-in-cell direct simulation Monte Carlo (PIC-DSMC) method. For the
Sang Hun Kang
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Temperature gradient in Hall thrusters [PDF]
Plasma potentials and electron temperatures were deduced from emissive and cold floating probe measurements in a 2 kW Hall thruster, operated in the discharge voltage range of 200–400 V. An almost linear dependence of the electron temperature on the plasma potential was observed in the acceleration region of the thruster both inside and outside the ...
D. Staack, Y. Raitses, N. J. Fisch
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Plume interference effects of the racetrack-shaped anode-layer Hall thruster system
Plume interference effects on the discharge characteristics and thruster performance for two heads system were investigated to evaluate the optimum design of the Hall thruster cluster system using the anode-layer head.
Takeshi MIYASAKA +6 more
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