A 2-D axisymmetric fluid model of the plasma in the insert region of a hollow cathode is presented. The level of sophistication included in the model is motivated in part by the need to determine quantitatively plasma fluxes to the emitter surface. The ultimate goal is to assess whether plasma effects can degrade the life of impregnated inserts beyond those documented throughout the 30-50 year history of vacuum cathode technologies. Results from simulations of a 1.2-cm diameter cathode operating at a discharge current of 25 A, and a gas flow rate of 5 sccm, suggest that approximately 10 A of electron current, and 3.5 A of ion current return to the emitter surface. The total emitted electron current computed by the model is about 35 A. Compa...
The discharge characteristics of hollow cathode directly affect the performance of thruster. In orde...
Abstract: Conditioning of the insert inside a hollow cathode is believed to be important to ensure r...
The use of electric propulsion in spacecraft applications is rising globally. The modeling of hollow...
A 2-D axisymmetric fluid model of the plasma in the insert region of a hollow cathode is presented. ...
In this paper, we present the first results from a Hollow Cathode Thermal (HCThermal) model that use...
Hollow cathodes have been used to sustain the discharge of Hall Effect Thrusters and ion thrusters f...
For many years research on hollow cathodes for Hall thrusters was focused only on the internal part ...
A zero-dimension plasma model of thermionic hollow cathodes is here derived. The equations of conser...
The Hollow Cathode (HC) is an electron source device that is widely adopted in electric propulsion s...
Thermionic hollow cathodes are currently used as sources of electrons in a variety of space applicat...
A model to predict the plasma properties inside a thermionic hollow cathode as a function of operati...
A particle and energy balance model of orificed hollow cathodes was developed to assist in cathode d...
Thermionic hollow cathodes are currently used in a wide variety of applications, including electric ...
In most gridded electrostatic thrusters, a single, centrally located hollow cathode supplies the e l...
This thesis presents experimental and modelling research on atmospheric pressure hollow cathodes and...
The discharge characteristics of hollow cathode directly affect the performance of thruster. In orde...
Abstract: Conditioning of the insert inside a hollow cathode is believed to be important to ensure r...
The use of electric propulsion in spacecraft applications is rising globally. The modeling of hollow...
A 2-D axisymmetric fluid model of the plasma in the insert region of a hollow cathode is presented. ...
In this paper, we present the first results from a Hollow Cathode Thermal (HCThermal) model that use...
Hollow cathodes have been used to sustain the discharge of Hall Effect Thrusters and ion thrusters f...
For many years research on hollow cathodes for Hall thrusters was focused only on the internal part ...
A zero-dimension plasma model of thermionic hollow cathodes is here derived. The equations of conser...
The Hollow Cathode (HC) is an electron source device that is widely adopted in electric propulsion s...
Thermionic hollow cathodes are currently used as sources of electrons in a variety of space applicat...
A model to predict the plasma properties inside a thermionic hollow cathode as a function of operati...
A particle and energy balance model of orificed hollow cathodes was developed to assist in cathode d...
Thermionic hollow cathodes are currently used in a wide variety of applications, including electric ...
In most gridded electrostatic thrusters, a single, centrally located hollow cathode supplies the e l...
This thesis presents experimental and modelling research on atmospheric pressure hollow cathodes and...
The discharge characteristics of hollow cathode directly affect the performance of thruster. In orde...
Abstract: Conditioning of the insert inside a hollow cathode is believed to be important to ensure r...
The use of electric propulsion in spacecraft applications is rising globally. The modeling of hollow...