A model to predict the plasma properties inside a thermionic hollow cathode as a function of operational conditions and geometry is presented. The hollow cathode features a lanthanum hexaboride (LaB6) insert, which is capable of emitting current densities as high as 10(5) Am-2 at temperatures of similar to 1900 K, along with a tantalum orifice plate located at the downstream end of the cathode tube. The model self-consistently computes the plasma parameters in both the emitter and orifice regions. A simple semiempirical relation is suggested to evaluate the plasma penetration depth in the cathode interior, which is of primary importance to establish the plasma conditions. The heat transfer mechanisms and the related temperature gradients al...
UnrestrictedThis research addresses several concerns of the mechanisms controlling performance and l...
A 2-D axisymmetric fluid model of the plasma in the insert region of a hollow cathode is presented. ...
Hollow cathodes are one of the main life-limiting components in ion engines and Hall thrusters. Alth...
Thermionic hollow cathodes are currently used in a wide variety of applications, including electric ...
Thermionic hollow cathodes are currently used as sources of electrons in a variety of space applicat...
Lanthanum Hexaboride (LaB6) hollow cathodes have been found in electric propulsion applications sinc...
Thermionic hollow cathodes are currently used as sources of electrons in a variety of space applicat...
Abstract: A new laboratory model lanthanum hexaboride (LaB6) hollow cathode sized for a 20 A HET dis...
In this paper, we present the first results from a Hollow Cathode Thermal (HCThermal) model that use...
Hollow cathodes are electron-emitting devices mainly used in Hall and Ion thrusters to ionize the pr...
The applications of electric propulsion are widely increasing in commercial and scientific missions ...
Self-heating hollow cathodes are central components in modern electric thrusters. The plasma dischar...
A 2-D axisymmetric fluid model of the plasma in the insert region of a hollow cathode is presented. ...
A zero-dimension plasma model of thermionic hollow cathodes is here derived. The equations of conser...
A particle and energy balance model of orificed hollow cathodes was developed to assist in cathode d...
UnrestrictedThis research addresses several concerns of the mechanisms controlling performance and l...
A 2-D axisymmetric fluid model of the plasma in the insert region of a hollow cathode is presented. ...
Hollow cathodes are one of the main life-limiting components in ion engines and Hall thrusters. Alth...
Thermionic hollow cathodes are currently used in a wide variety of applications, including electric ...
Thermionic hollow cathodes are currently used as sources of electrons in a variety of space applicat...
Lanthanum Hexaboride (LaB6) hollow cathodes have been found in electric propulsion applications sinc...
Thermionic hollow cathodes are currently used as sources of electrons in a variety of space applicat...
Abstract: A new laboratory model lanthanum hexaboride (LaB6) hollow cathode sized for a 20 A HET dis...
In this paper, we present the first results from a Hollow Cathode Thermal (HCThermal) model that use...
Hollow cathodes are electron-emitting devices mainly used in Hall and Ion thrusters to ionize the pr...
The applications of electric propulsion are widely increasing in commercial and scientific missions ...
Self-heating hollow cathodes are central components in modern electric thrusters. The plasma dischar...
A 2-D axisymmetric fluid model of the plasma in the insert region of a hollow cathode is presented. ...
A zero-dimension plasma model of thermionic hollow cathodes is here derived. The equations of conser...
A particle and energy balance model of orificed hollow cathodes was developed to assist in cathode d...
UnrestrictedThis research addresses several concerns of the mechanisms controlling performance and l...
A 2-D axisymmetric fluid model of the plasma in the insert region of a hollow cathode is presented. ...
Hollow cathodes are one of the main life-limiting components in ion engines and Hall thrusters. Alth...