A 200 W No-Wall-Losses Hall Thruster (NWLHT-200 W) is designed and processed to verify the technology of pushing down magnetic field with two permanent magnetic rings. To create a magnetic field, NWLHT-200 W uses two permanent magnetic rings (inner and outer) in the absence of magnetic screen or magnetic component. The anode is at the internal magnetic separatrix position, and the thruster shell is hollow to enhance the heat dissipation of ceramics. The magnetic field strength at the channel outlet is 90% of the maximum magnetic field. In this study, the experimental results concerning the thrust, discharge current, specific impulse, and efficiency are presented and examined. Our experiments show that “no erosive discharge” of wall is achie...
This dissertation presents research aimed at extending the efficient operation of 1600 s specific im...
The performance and plume characteristics of a 2-k W Hall thruster with segmented anodes for thermal...
The performance of a low-power cylindrical Hall thruster, which lends itself more readily to miniatu...
The design of the magnetic field is crucial to the performance of the hall thruster. This paper inve...
This dissertation presents an investigation of the applicability of magnetic shielding to low-power ...
In recent times, there has been strong growth in the diffusion of Hall Thrusters, both as a main roc...
The performance of a low-power cylindrical Hall thruster, which more readily lends itself to miniatu...
Thrust performance and stable operation conditions of an anode layer type Hall thruster was investig...
Thrust performance and stable operation conditions of an anode layer type Hall thruster was investig...
Theoperation andperformance of amicro-Hall thruster are characterized.The thruster is coaxial in des...
Hall thrusters are one of the most used rocket electric propulsion technology. They combine moderate...
In steady-state operation of Hall thrusters excited by permanent magnets, the existence of temperatu...
This study adopts double permanent magnetic rings and four permanent magnetic rings to form two symm...
A series of numerical simulations and experiments have been performed to assess the effectiveness of...
A laboratory-model Hall thruster with a magnetic circuit designed for high-specific impulse (2000–30...
This dissertation presents research aimed at extending the efficient operation of 1600 s specific im...
The performance and plume characteristics of a 2-k W Hall thruster with segmented anodes for thermal...
The performance of a low-power cylindrical Hall thruster, which lends itself more readily to miniatu...
The design of the magnetic field is crucial to the performance of the hall thruster. This paper inve...
This dissertation presents an investigation of the applicability of magnetic shielding to low-power ...
In recent times, there has been strong growth in the diffusion of Hall Thrusters, both as a main roc...
The performance of a low-power cylindrical Hall thruster, which more readily lends itself to miniatu...
Thrust performance and stable operation conditions of an anode layer type Hall thruster was investig...
Thrust performance and stable operation conditions of an anode layer type Hall thruster was investig...
Theoperation andperformance of amicro-Hall thruster are characterized.The thruster is coaxial in des...
Hall thrusters are one of the most used rocket electric propulsion technology. They combine moderate...
In steady-state operation of Hall thrusters excited by permanent magnets, the existence of temperatu...
This study adopts double permanent magnetic rings and four permanent magnetic rings to form two symm...
A series of numerical simulations and experiments have been performed to assess the effectiveness of...
A laboratory-model Hall thruster with a magnetic circuit designed for high-specific impulse (2000–30...
This dissertation presents research aimed at extending the efficient operation of 1600 s specific im...
The performance and plume characteristics of a 2-k W Hall thruster with segmented anodes for thermal...
The performance of a low-power cylindrical Hall thruster, which lends itself more readily to miniatu...