A particle and energy balance model of orificed hollow cathodes was developed to assist in cathode design. The model presented here is an ensemble of original work by the author and previous work by others. The processes in the orifice region are considered to be one of the primary drivers in determining cathode performance, since the current density was greatest in this volume (up to 1.6 x 10(exp 8) A/m2). The orifice model contains comparatively few free parameters, and its results are used to bound the free parameters for the insert model. Next, the insert region model is presented. The sensitivity of the results to the free parameters is assessed, and variation of the free parameters in the orifice dominates the calculated power consump...
In this paper, we present the first results from a Hollow Cathode Thermal (HCThermal) model that use...
A preliminary numerical model has been developed as a first step toward the definition of a self-con...
Hollow cathodes have been used to sustain the discharge of Hall Effect Thrusters and ion thrusters f...
A zero-dimension plasma model of thermionic hollow cathodes is here derived. The equations of conser...
Thermionic hollow cathodes are currently used in a wide variety of applications, including electric ...
The research presented in this dissertation aims to scale orificed hollow cathodes for low-current e...
The Hollow Cathode (HC) is an electron source device that is widely adopted in electric propulsion s...
For many years research on hollow cathodes for Hall thrusters was focused only on the internal part ...
Peer Reviewedhttp://deepblue.lib.umich.edu/bitstream/2027.42/76725/1/AIAA-1998-3345-942.pd
<p>Prediction of hollow cathode orifice is one of the most important goals of a well performed desig...
Thermionic hollow cathodes are currently used as sources of electrons in a variety of space applicat...
A 2-D axisymmetric fluid model of the plasma in the insert region of a hollow cathode is presented. ...
A model to predict the plasma properties inside a thermionic hollow cathode as a function of operati...
A 2-D axisymmetric fluid model of the plasma in the insert region of a hollow cathode is presented. ...
The fidelity of electric propulsion physics-based models depends largely on the validity of their pr...
In this paper, we present the first results from a Hollow Cathode Thermal (HCThermal) model that use...
A preliminary numerical model has been developed as a first step toward the definition of a self-con...
Hollow cathodes have been used to sustain the discharge of Hall Effect Thrusters and ion thrusters f...
A zero-dimension plasma model of thermionic hollow cathodes is here derived. The equations of conser...
Thermionic hollow cathodes are currently used in a wide variety of applications, including electric ...
The research presented in this dissertation aims to scale orificed hollow cathodes for low-current e...
The Hollow Cathode (HC) is an electron source device that is widely adopted in electric propulsion s...
For many years research on hollow cathodes for Hall thrusters was focused only on the internal part ...
Peer Reviewedhttp://deepblue.lib.umich.edu/bitstream/2027.42/76725/1/AIAA-1998-3345-942.pd
<p>Prediction of hollow cathode orifice is one of the most important goals of a well performed desig...
Thermionic hollow cathodes are currently used as sources of electrons in a variety of space applicat...
A 2-D axisymmetric fluid model of the plasma in the insert region of a hollow cathode is presented. ...
A model to predict the plasma properties inside a thermionic hollow cathode as a function of operati...
A 2-D axisymmetric fluid model of the plasma in the insert region of a hollow cathode is presented. ...
The fidelity of electric propulsion physics-based models depends largely on the validity of their pr...
In this paper, we present the first results from a Hollow Cathode Thermal (HCThermal) model that use...
A preliminary numerical model has been developed as a first step toward the definition of a self-con...
Hollow cathodes have been used to sustain the discharge of Hall Effect Thrusters and ion thrusters f...